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        ATMOSPHERIC THERMODYNAMICS HP48 Calculator Program
         Contents
1.   Enter P  C  U  W v  air saturation enthalpy at  water temperature and enthalpy of surface air  Dalton Equation plus Im spray  term     Enthalpy transfer coefficient from   CD   0 7  Ooyama  1969  and CBLAST  Drag coefficient from Ooyama  1969    CE to CD Ratio   0 7 from CBLAST   Drag coefficient according to Dalton   0 0018 from CBLAST   Drag coefficient according to Powell   0 002 from CBLAST   Spray power of five heat transfer coefficient     Hurricane total heat from sea removal rate from ocean cooling in Watt Enter     32    QHU    QHV    DREN    AT Ocean cooling due to hurricane passage    C   d Depth of cooled layer  m    w Width of cooled layer  m    v Velocity of hurricane  m s    Result is total sea to air heat transfer in watts    Assumes all cooling occurs under eyewall     Hurricane heat removal rate per unit area of eyewall  W m      Enter   Hurricane total heat from sea removal rate  result of QHT      Eyewall length   w Eyewall width   Result is eyewall sea to air heat transfer in W m        Hurricane heat required to produce hurricane precipitation   Enter rain rate in mm hr  and diameter of rain area in meters    Heat flux from eddy calculation  Enter CE  U10  Q0 and Q10  Results are  lt w   q    gt   and Qv  Used Drennan eddy correlation heat flux calculation in Table 1 of French  and Drennan     Part1  2007    Heat from sea removal rate    RAY    GR    Rayleigh Number for free convection of air in a tube     enter  Delta T  mean T   Diameter  Grashof Num
2.   GCK    TMS    PRO2  PRO3    ASA  ASW  ApA  AuW    WI  THE  TCE  F1  TPLT  RPLT  TVL1    Gibb free energy check after running WTUW   no parameters required just press  SCK entered   Results consist of four numbers    Gibb free energy of gas phase in final state   Gibb free energy of liquid phase in final state   Gibb free energy of gas phase in initial state   Gibb free energy of liquid phase in final state  Change in total Gibb free energy is the maximum energy that would be produced  if the mixing process were carried out reversibly     Calculates the property of a mixture of mass  1 and of the MM2 water part of  mass  2 where MM2 is in vapour state  TT2 and MM2 are used to specify the  quantity of vaporized water added to the humid air mass  PP2 is ignored     Surface pressure capability of saturated air water mixture   Surface pressure capability of air water mixture     Change in entropy of air during mxing     Change of entropy of water during Mixing     Change in free enthalpy     For two air masses mixture   Change in free enthalpy     For air and condensed water mixture    Work loss due to irreversible heating  Effective temperature of the hot source  Effective temperature of the cold source  Fraction air mass  1   Plots the virtual temperature of the mixture array     Plots the relative humidity of the mixture array        AT5C Margules large air mass    ZPO    MA Alpha    MA Theta    W Theta TZ    1  Two forms of the Margules equations for calculating the total en
3.   K V   1990  A thermodynamic foundation for modelling the moist atmosphere   J  Atmos  Sci   47  2580 2593     Lilly  D K   T  Gal Chen  1990  Can dryline mixing create buoyancy  J  Atmos  Sci   47   1170 1171     46    
4.  adiabatid expansion      Default 1000 J kg    HCU1 Isabel Distant environment surface air conditions     101 1 kPa  27 8   C  75  RH   HCU2 Jordan sounding surface air for which WB is zero for P4   12 kPa  101 1 kPa  27 8   C  63 8  RH   HCU3 Jordan sounding surface air for which WB is zero for P4   12 kPa  101 1 kPa  28   C  62 63  RH   HCM4 Jordan sounding surface air for which T4   T4E for P4   12kPa  101 51 kPa  31 09   C  17 79 g kg   HCM5 Jordan sounding surface air for which T4   T4E for P4   13kPa  101 51 kPa  26 25   C  17 79 g kg   PC     PJ Jordan sounding base pressure    AdJ1__ Subdirectory of AT5J  Pressure at solar chimney top     P200  P1K    A5J2 _Subdirectory of AT5J     Work correlations moved out of AT5J  W2U Equation derived from correlation for calculating work produced when surface air is    raised reversibly to the 20 kPa level without need for using slow solver   Enter surface  air conditions in PCU format      38    W2M    Equation derived from correlation for calculating work produced when surface air is  raised reversibly to the 20 kPa level without need for using slow slover   Enter surface  air conditions in PCM format      TEE MPI from SST   Isabel correlation   DEM MPI from SST   Isabel correlation   EMA MPI from SST   Emanuel correlation    APE Calculate delta P from CAPE      APM Calculate turbine delta P given P1  K1  W12  M1   A5J3 _ Total work calculations   VDT Enter upward velocity  V  at the base of chimney and chimney diameter D    ca
5.  and press the  corresponding key  Irrespective of which three parameters are entered the properties are  returned to the stack in the PKM format  Pressure is stored in variable PP  absolute  temperature in variable TT  and mixing ratio is stored in variable MM     MM is the total quantity of water per unit mass of air  the mixing ratio  MM includes the water in  any phase  its unit is g water kg air  Water beyond the saturation amount is considered to be in  a condensed phase and in equilibrium with the air  If there is condensed water  the water in the  vapour phase is the saturation amount  The condensed water is in the liquid phase if the  temperature is above the freezing temperature TF  Properties per unit mass of dry air  mixing  ratio  are used in preference to properties per total mass of substance because in many  processes air content is conserved while water content can change   for example in processes  where condensed water is separated from expanding air  pseudo adiabatic expansion   Open  pseudo adiabatic expansion is handled by removing the condensed water at regular interval     Example   Pressure  P   0 kPa  Dry Bulb Temperature C   20  C  Dew point  D 15  C  PP 90 kPA  TT 293 15 K  MM 12 00 g kg    Arguments  3 90 2 20 1 15  Function  PCD  Results  3 90 2 293 15 1 12 00    Program  R  recalls the three standard properties to the stack  Calculation of the  thermodynamic properties is based on having the three standard air property variables on the  stack an
6.  from Holland 1997   OL Potential temperature   PL Lifting condensation level pressure   TL Lifting condensation level temperature    Expansion temperature is calculated in step of 2 kPa  Condensed water is separated after each  step  Freezing temperature is set to  100   C  the condensed water does not freeze  A P4  default of 10 kPa is sufficient to reduce water content to negligible level  Pseudo adiabatic  expansion temperatures at intermediate pressures can be calculated by varying P4 in which  case 0e is not valid  TPSE calculation requires up to 40 solver operation and can take   30 seconds to run on a fast PC     44    AT5P Sounding array and array conversion programs    The AT4 directory contains five arrays of sounding data     SNK Sounding data in PKM format  SNKU Sounding data in PKU format  SNC Raw sounding data in PCD format  SNCM Raw sounding data in PCM format  SNU Sounding data in PCU format    There are five programs to store and generate the five arrays     K gt U Generate SNU from SNK  KU gt K Generate SNK from SNKU  K gt C Generate SNC from SNK  C gt K Generate SNK from SNC  U gt K Generate SNK from SNU  CM gt K Generate SNK from PCM    AT6 __ Plot using MLINE    AT6 uses program MLINE of AT1 to plot the date in the arrays of AT5  The array to be plotted  is stored in array DA    The samples in the directory can be copied and modified to plot other properties  Plotting  range and axis labelling can be redefined     The built in plots are     PPLT Pseudo a
7.  from P1 and p2     Carnot efficiency from Th and Tc in   C  Carnot efficiency from Th and Tc in K  Mole fraction from m    Ratio mass of air to total mass from M   Mixing ratio to specific humidity  Specific humidity to mixing ratio    Restrained and unrestrained cylinder piston system  Inputs  P1  P2  T1  in   C     Van Ness type analysis   Outputs  initial temperature  isentropic expansion  temperature  and unrestrained expansion temperature  RPN version    Same as POP  Algebraic version   Restrained and unrestrained cylinder piston system  Input pressure ratio  P2 P1    Output  Percent of isentropic expansion work loss as a result of the expansion not  being fully restrained  Note  The loss work is 23 63  for P2 P1 of 0 95 and  approaches 22 25  as P2 P1 approaches 1  i e  0 999     Potential temperature lapse rate from P and lapse rate  Potential temperature lapse rate from 9  T        Vapor pressure of water in kPa     slightly more accurate than XVL  Affinity A   0  Vapor pressure of water in kPa     slightly more accurate than XVI  Affinity A   0  Vapor pressure of water in kPa     slightly less accurate than PVL  Dufour eq  9 87  Vapor pressure of water in kPa     slightly less accurate than PVI  Dufour eq  9 87    NNN  N    21    AT3A_ CLAPEYRON EQUATION COEFFICIENTS  from Dufour and Van Mieghem   AT3B SOLAR AND INFRARED RADIATION    AT3B contains the nominal percent of radiation reflected and absorbed by the atmosphere and  the earth surface  the solar constant  th
8.  primary directory AT4    AT2 Thermodynamic constants     AT3 Thermodynamic properties of pure air and pure water  virtual  temperature  lapse rate  and the distance between sounding pressure    AT4    AT5    AT6    levels     Thermodynamic properties of moist air  The condition of the unit mass of air is  specified by entering pressure  temperature  and a humidity parameter  The  directory uses the HP48 solver to calculate adiabatic expansion temperature   dew point  wet bulb  and equivalent temperature     Thermodynamic properties of complete soundings and work produced when air  masses are moved     Programs to plot data from arrays     2 3 Side sub directories    Side sub directories are used where the data is not likely to be used further down  The name of  side directories terminates with a letter     AT2A  AT2B  AT2C  AT2D  ATDAT    AT3A  AT3B    AT3C  AT3D  AT3E    AT4A  AT4B  AT4C    AT5A    AT5B  A5B1 A5B4    A5B1  A5B2  A5B3 A5B4  A5B6    A5B7  A5B8  AT5C    Energy usage and reserves  Conversion MPG to Km hr to L 100 km  Energy cost   Hurricane categories and velocities  Atmospheric sounding data    Clappeyron equation coefficients calculation    Constants relating to the Earth energy budget  percent of radiation reflected  and absorbed by the atmosphere and the earth surface  the solar constant  the  Stefan Boltzman law  and conversion factors from Langley    Thermodynamic properties of propane    Circulation from earth rotation   Lambton College Prototype Paramet
9.  properties of a mixture of two air masses or of a mixture of an air mass  and of condensed water  Mixing is an isenthalpic process     The calculation is based on the fact that the enthalpy of the mixture and the water content of  the mixture must be equal to the sum of the enthalpy and water content of the initial masses     The program is primarily intended air masses initially at the same pressure but can also be  used for air masses at different pressures provided M2 has the higher pressure  The pressure  of the mixture is the lowest of P1 and P2  The higher pressure air mass in expanded  isentropically before mixing  Air masses can have water in condensed states     PCU1  PCU2  PCM1  PCM2  RC1  RC2  RC3    RK1  RK1    PCT1  SIA    PCTA    DA    TMW    SAW    WTW    WTU    WTUW    Stores properties of air mass  1 in PCU format in PP1  TT1  and MM1   Stores properties of air mass  2 in PCU format in PP2  TT2  and MM2   Stores properties of air mass  1 in PKM format in PP1  TT1  and MM1   Stores properties of air mass  2 in PKM format in PP2  TT2  and MM2     Recall air mass  1 properties in PCM format  Recall air mass  2 properties in PCM format  Recall air mass  3 properties in PCM format    Recall air mass  1 properties in PKM format  Recall air mass  2 properties in PKM format    Calculates mixture property given percent of mass  1   Calculate mixing internally generated entropy  mix air masses 1 and 2     Produces an array DA of mixture properties at 10  mass  1 incre
10.  temperature  TF     Freezing temperature TF  default 273 15 K  and freezing band FB  default 20 K  are stored in  constant directory AT2 and can be changed to check their effect  The freezing band must be at  least 5 K to avoid solver singularity problem    AT4 HP48SX SOLVERS    The HP48 solver is used to solve for variables that cannot be isolated and to avoid having to  manipulate equations     Program  S EQ  is an equation calculating the total entropy from PP TT  and MM  The  temperature during true adiabatic expansion is calculated by entering PP and solving for TT   Program TSOL invokes the solver to solve for TT given PP     The MEQ directory contains the following equations     A EQ Entropy moisture is condensed    E EQ Enthalpy moisture content condensed   EM EQ Enthalpy Emanuel PKM equation  EU EQ Enthalpy Emanuel PKU equation  G EQ Gas Law    H EQ Enthalpy    L EQ Humidity minus 100  Used by LCL3 to calcualte lifting condensation level   M EQ Entropy for two conditons equation  S EQ Entropy    TV EQ Virtual temperature equation   V EQ Vapour Pressure    W EQ Enthalpy at Wet Bulb    W2 EQ    Enthalpy  amp  wet bulb    The solver will solve for any missing variable  The following programs invoke the solver directly  to calculate frequently need variables     ASOL Isentropic desiccation temperature   enter P   Solve A EQ    DSOL Dew Point Temperature   enter partial pressure of water   Solve the V EQ  HSOL Mixture temperatures   Enter P   Solve H EQ  for TT   USOL So
11. 37 m       AD Area of 8   6    x 24    tangential deflector entry slots     0 74 m   AF1 Heat capacity of small salamander 44 000 W   AF2 Heat capacity of large salamander 110 000 W   ARD   Ratio of diamerter     3 89   ARV   Ratio of velocity     0 15     AS1 Area of 8   6    x 24    tangential deflector entry slots  AT4 MAIN PROGRAM   See description at beginning of program description  AT4A_   Subsidence velocity    AT4B      23    AT4C_ EFFICIENCY OF COMBINED CYCLES  Efficiency calculations for three stages combined cycle  Gas turbine  steam  AVE  Cycles can  be omitted by making hot and cold source temperatures the same     TSTO Store up to four source temperatures in   C  Example 1600  600  30   50    TRCL Recall up to four source temperatures in   C   COTA Calculate actual cycle efficiency  initiates COMN   COMT Calculate Carnot efficiency  initiates COMN   COMP Calculate percent contribution of each cycle and percent increment due to AVE  cycle   COMW Display W1  W2  W3  W4    COMN Calculate percent contribution of each cycle from individual efficiency  enter the  three efficiencies from COTA or COMT  delete x   Also calculate W1  W2  W3   W4    EFF Carnot efficiency     Enter Th and Tc in   C   EFF2 Carnot efficiency     Enter Th and Tc in   C with exchanger Delta T   EFH Carnot efficiency     Enter Th in K and use default TH   EFF Carnot efficiency     Enter Tc in K and use default TC   EFU Ultimate efficiency when work is dissipated at hot source temperature      E
12. 5   TQ Triple point temperature  273 16    Flags 1 and 2 are used to set Freezing Temperature    Flag 3 is used to set Freezing Band    Flags are used because the flag status is visible in the calculator screen and because flags can  be changed from any directory while objects can only be stored in the current directory       Toggle between freezing temperature of 273 15 K  Ice   Flags 1 and 2 clear   and 173 15 K  No Ice     Flags 1 and 2 set    II Toggle between freezing bans of 20 K  flag 3 clear  and freezing band of  5 K  Flag 3 set     SFT Set Freezing Temperature  TF Freezing temperature  273 15 K  F1 F2 TF SFT argument  Clear Clear 0   C 0  Set Clear  10   C 10  Clear Set  40   C 40  Set Set  100  C 100    The Freezing Temperature can be selected by setting the flags manually or by preceding the  the SFT object with the argument of the above table     FB Freezing band  20 K    The Freezing Band can be selected by setting flag 3 manually or toggled by pressing the SFB  without argument  The default FB with flag 3 clear is 20  FB is 5 when flag 3 is set     CPA Specific heat of air at constant pressure   CVA Specific heat of air at constant volume   RA Gas constant for air   KA RA CPA   MA Molecular weight of air   CPV Specific heat of water vapour at constant pressure  RV Gas constant for water vapour   CW Specific heat of water   CI Specific heat of ice   LVO Latent heat of vaporization at TO   LVQ Latent heat of vaporization at the triple point of water  LFO Latent h
13. ATMOSPHERIC THERMODYNAMICS  HP48 Calculator Program Documentation  Louis Michaud  Revised  October  2015    1 0 PROGRAM DESCRIPTION    HP48 calculator program Atmospheric Thermodynamics  AT1  calculates the properties of air  containing water in any phase  given pressure  temperature and a humidity parameter  The  program can calculate a wide range of parameters including    Thermodynamic properties for individual air masses or of complete sounding    Work produced when small air masses are moved isentropically    Work produced when large masses of dry air change position    Properties of mixtures of air and water    Pressure drop and work loss for laminar and turbulent flow in tubes  work loss and  terminal velocity for bubble flow     OIE    The program uses the power and versatility of the Hewlett Packard HP48 object oriented  programming language  The HP48SX calculator came out in 1990 and is now out of  production  The HP48SX is a programmable scientific calculator using object oriented  programming  programmable keys  Reverse Polish Notation  RPN  or Algebraic Notation   When it came out the HP48SX was the leading scientific calculator and has not been  surpassed  A community of HP48SX adepts developed  When HP stopped producing the  calculator the community developed an HP48SX emulator for PC   s which is available free of  charge on the internet  The PC emulator runs approximately 100 times faster than the original  calculator on a medium speed desktop  A calculation 
14. D  PTAZ  PCAZ  TPTA    Z EQ  PX1  PX2  CX1  ax    Partial pressure of water from P and M    Partial pressure of air from P and T  dew point     Saturation mixing ratio from P and T      Vapor in equilibrium with liquid or ice  Saturation mixing ratio from P and T      Vapor in equilibrium with liquid    Density of pure air from P and T  Density of pure water from P and T    Entropy of air from P and T per kg air    Entropy of vapour from P and T per kg vapour    Entropy of liquid water from T per kg liquid water   lower case to distinguish from  built in    shift left       Entropy of liquid water from P  T  M per kg of water  Uses sL and throws out P and    Entropy of ice from T per kg of ice    Entropy of condensed water from T per kg liquid water    Entropy of condensed water from P  T  M per kg of water  Uses SC and throws out P  and M     Enthalpy of air from T per kg air    Enthalpy of vapour from T per kg water    Enthalpy of liquid water from T per kg water    Enthalpy of ice from T per kg ice    Enthalpy of condensed waater from T  per kg water    Enthalpy of condensed water from P  T  M  per kg of water  Uses HC and throws out  P and M     Free enthalpy of air from P and T per kg air    Free enthalpy of vapour from P and T per kg vapor   Free enthalpy of liquid water from T  per kg water   Free enthalpy of ice from T  per kg ice    Affinity of liquid water from P and T     Virtual temperature from T and M   Latent heat of vaporization from t   Latent heat of sublima
15. ELZARA     10000  25 m  20   C  40 m s   ZARA ELZARA     150  60 m  20   C  8 m s   GR1 Grotvlei     120 m  83 m  31 5   C  2 07 m s  9 75   C km   GR2 Grotvlei     120 m  83 m  31 5   C  2 07 m s  6 5   C km   GR20 Grotvlei     2400 m  83 m  31 5   C  2 07 m s  6 5   C km   GR21 Grotvlei     2400 m  17 m  30 5   C  50 m s  6 5   C km   GR21 Grotvlei     2400 m  30 m  15   C  30 m s  6 5   C km   GT Grptvlei     120 m  58 m  31 5   C  4 24 m s  6 5   C km   AT5N_ PSEUDO ADIABATIC EXPANSION TEMPERATURE AND EQUIVALENT   TEMPERATURE   PKM1 Enter initial air properties in PKM format store in P1  T1  M1   PCM1 Enter initial air properties in PCM format store in P1  T1  M1   PCU1 Enter initial air properties in PCU format store in P1  T1  M1   P4 Enter final pressure  default 10 kPa    TOEN Calculate pseudo adiabatic expansion temperature and equivalent temperature  No argument required  Results are final temperature in   C  in K  and 0e   No freezing of condensed water     Freezing temperature 173 15 K    TOEF Calculate pseudo adiabatic expansion temperature and equivalent temperature  No argument required  Results are final temperature in   C  in K  and 8e  With  With freezing of condensed water     Freezing temperature 273 15 K    0 33 Equivalent temperature based on raising air to 10 kPa level    Os eq Equivalent potential temperature equation     no separation   SL3 Entropy when water is in liquid phase   BOL3 Equivalent temperature using Bolton equation   BOL4 Bolton equation
16. I  Note that T4 is higher in the irreversible case than in the reversible case by  Wosrev  Cpa     Convection Energy with heater humidifier    WA2 _ Calculate P3 given T3 and U3   WA Calculate reversible work for entered for P3 guess  given T3 and U3   Wet heat     TU Enter temperature and relative humidity downstream of heater humidifier before running  WA or WA2   WA2 Calculate P3 using two guesses method  given T3 and U3  Provide one P3 guess    WD2_ Calculate P3 given T3 and M3   WD Calculate reversible work for entered for P3 guess  given T3 and M3   Dry heat     TM Enter temperature and mixing ratio humidity downstream of heater humidifier before  running WD or WD2   WD2 Calculate P3 using two guesses method  given T3 and M3  Provide one P3 guess    WTA2 Calculate C3 required to produce work given WO and U3   WTA Calculate work for temperature C3  in   C  given WO and U3  Provide C3 guess     WU Enter work of buoyancy  WO  and relative humidity  RH3  in state 3 before running WTA  or WTA2  Set WO to zero to find datum temperature for which W   0    WTA2 Calculate C3 required to make the work zero given U3 using two guesses method   Provide C3 guess      OK for zero work   Needs fixing when work  gt  0     WUA2 Calculate relative humidity required to produce work given WO and T3   WUA Calculate relative humidity given WO and C3  Provide relative humidity guess     WC Enter work of buoyancy  WO  and temperatrue  T3  in state 3 before running WUA or  WUA2  Set WO0 to zero 
17. JR  DJV    ATMC  MAN  MAN2  EMI  EMI2    Enter height and base temperature in    C   caculates efficiency from simple solar  chimney equation    Enter chimney height  Z   chimney base temperature    C   and chimney base  delta T  AT   Calculate ideal work per unit mass  J kg  from simple solar  chimney equation    Ex  Manzanares 200 m  30  C  17  C   gt  109 91 J kg    Pressure  kPa   Temperature  K   Mixing ratio  g kg     Adrian Bejan Work equation   Adrian Bejan Power equation   Flatness Factor used in DJV   Diameter of Rankine vortex based on radial delta P    Input Conditons for various cases   Manzanares     200 m  10 m  20   C  8 m s  Manzanares     1000 m  10 m  3 4   C  8 m s  EnviroMission     1000 m  150 m  28   C  16 m s  EnviroMission     1000 m  180 m  20   C  16 m s    43    DEV2 Dust Devil     1000 m  2 m  5   C  12 m s   DEV10 Dust Devil     1000 m  10 m  5   C  12 m s   FWH Fire Whirl     1000 m  2 m  100   C  20 m s   ESC Eskom AVE     10 000 m  50 m  20   C  20 m s   DCT Dry cooling tower     10 000 m  35 m  20   C  20 m s   DCT8 Dry cooling tower     10 000 m  18 m  20   C  80 m s   DCT    Dry cooling tower     10 000 m  35 m  20   C  20 m s  8 09   C km   DCT Dry cooling tower     10 000 m  18 m  20   C  80 m s  8 09   C km   DCTs Dry cooling tower     2 000 m  35 m  20   C  20 m s  5   C km   KEN Kendall  Eskom    165 m  145 m  20   C  4 m s   GAR Garage prototype     2 m  0 05 m  100   C  1 m s   LAM Lambton College   5 m  0 25 m  30   C  5 m s   ZARV 
18. L  RE  REW    FL  FT   FTW  FLW    Work loss  J kg  for turbulent and laminar flows  Enter DVZp    Work per unit mass loss through friction in a horizontal tube for laminar air   From  d  v  z  rho    Work per unit mass loss through friction in a horizontal tube for turbulent air   From  d  v  z  rho     Circular conduit area from  d   Volumetric flow  m3 s   from d  v    Mass flow  kg s   from d  v rho   Reynold number for turbulent air  From d v rho   Reynold number for water  From d  v  rho     Friction Factor laminar flow    Friction Factor turbulent flow air  From d  v  rho   Friction Factor turbulent water  From d  v  rho   Friction Factor laminar water  From d  v  rho     Buoyant air bubble flow     FBUO  FDRG  DDRG  WDRG  VTER  VJS  SVOL  SMAS  CD    CK    HFX    HFS    HFSA    CEO  CDO  CEDR  CDD  CDP  CS    QHT    Buoyancy force from  d  rho ambient  b  b rho ambient     rho parcel  Drag force from  d  v  rho        Drag work from  d  v  Z    Terminal velocity from  d  b        Sphere volume   Sphere mass   Drag coefficient  constant   0 5     Sea to Air heat transfer coefficient  Enter v     Sea to Air heat transfer  in W m    Enter p  air density   hs  air saturation  enthalpy at water temperature   ha  air enthalpy   v  velocity    Dalton equation  Sea to Air heat transfer  in W m    Enter p  air density   hs  air saturation  enthalpy at water temperature   ha  air enthalpy   v  velocity    Dalton equation  plus Im spray term    Sea to Air heat transfer  in W m  
19. N  WX  WF  and WT  FF Vortex mode friction loss multiplier  default   10   VF Vortex mode exit velocity divider   default   10   THP Calculate enthalpy and entropy   ENR Calculate heat  work  average source temperatures  and efficiency   HYD Calculate air density   Z4 Chimney height   T Lapse rate   VCH Upward velocity at the bottom of the chimney   DCH Chimney diameter   DCO Diameter of collector  ie 244 m    FCO Heat flux on collector  ie 800 W m2    NCO Efficiency of collector  ie 31     NT Turbine efficiency in    default 80     p2 Density of air at the base of the collector outlet   P1 P4 Pressures  kPa    T1 T4 Temperatures  K    H1 H4 Enthalpies  J kg     1 S2 Entropy  J K kg     u3 u4Moist static energy    Specific work    wl Specific work     ideal reversible J kg    wX Specific work     Turbine loss  J kg    wF Specific work     Friction loss  J kg    wT Specific work     Turbine loss  J kg    wC Specific work     Work of compression  J kg   wE Specific work     Work of expansion  J kg   Total work   QQI Heat input  W    WI Ideal work  W    WN Net work  W    WX Exit losses  W    WF Friction losses  W    WT Turbine losses  W    Specific heat   QI Heat in  J kg    QO Heat out  J kg    EF  Efficiency   TCA Effective temperature of the cold source  THA Effective temperature of hot source   D400 Manzanares velocity delta T correlation at 400 W m  insolation  D800 Manzanares velocity delta T correlation at 800 W m  insolation    42    HT    HTAT    PP    MM    BJW  BJP  D
20. PB5    GST  GSP    ZB    WKT    o EQ  oSOL    AVS  AVH  AVM    Kinetic Energy produced when a parcel from base level is raised true  adiabatically to pressure P  Enter upper level P  Kinetic energy equals total  energy minus WPP    Kinetic Energy when the parcel is moved to another sounding level  Enter upper  level row number  Kinetic energy equals total energy minus WPP     Kinetic Energy produced when a parcel recalled using Alpha GET is raised true  adiabatically to pressure P   The work becomes positive at the Level of Free  Convection  LFC    Kinetic energy equals total energy minus WPP     Potential energy of condensed water for typical pseudo adiabatic expansion   default value 1000 J kg     Total Mechanical Energy produced when a parcel from base level is raised true  adiabatically to pressure P  Enter upper level P    Total Mechanical Energy produced when the parcel is moved to another  sounding level  Enter upper level row number    Total Mechanical Energy produced when a parcel recalled using Alpha GET is  raised true adiabatically to pressure P   The work becomes positive at the Level  of Free Convection  LFC      Sounding in PCD format   Sounding in PKM format   Sounding in PKM plus elevation  Sounding     True adiabatic expansion  Sounding     Pseudo adiabatic expansion    Generate soundings al  GST GSP I  Generate sounding heights    Toggle between reversible  constant entropy  and irreversible   constant static energy  expansion by setting flag 4    Pressure 
21. YPPH PPH steam to Watt   ZPPH Watt to PPH steam   YQPY  Quadrillion BTU yr to Watt   ZQPY Watt to quadrillion BTU yr   YTR Ton of refrigerant to Watt   ZTR Watt to Ton of refrigerant   YHR Heat Rate to Efficiency   ZHR Efficiency to Heat Rate  BTU kW hr   Energy Conversion   YMO Cubic meter of crude oil to Joule  ZMO Joule to cubic meter of crude oil  YMG Cubic meter of natural gas to Joule  ZMG Joule to cubic meter of natural gas  YBBL Barrel of crude to Joule   ZBBL Joule to barrel of crude oil    12    YTOE  ZTOE  YTC  ZTC  ZTNT  YTNT    Tonne of crude oil to Joule  Joule to tonne of crude oil  Tonne of coal to Joule  Joule to tonne of coal  Joule to tonne of TNT  Tonne of TNT to Joule    Miscellaneous conversions    TO B  B TO  G   KG  KG gt G  GP  PG  KS gt G  GM    gt K  CF  gt KG  KG   KCF  pM  plo    Tonne of crude oil to barrel   Barrel of crude oil to tonne   US gallons to kilogram of water   Kilogram of water to US gallon   US gallon of water to pound   Pound of water to US gallon   Kilogram per second water to US gallon per minute  US gallon per minute water to kilogram per second  Standard cubic feet of air to kilogram   Kilogram of air to standard cubic feet   Density lb ft  to kg m     Density kg m  to lb ft       Conversion Factors    WPH  WQ  WTR  BKH  GP  JMO  JMG  JTOE  JBBL  JTC  JTT  TOB    Watts per pound per hour steam  Watts per quadrillion BTU per year  Watt per ton of refrigerant   BTU per kilowatt hour   Pound per Gallon   Joule per cubic meter of o
22. a     QO  O  Z  3  5    OF a Oli Gas    Content   Pressure  kPa    Temperature  K    Mixing ratio  g kg    Entropy  J kg K    Virtual Temperature  K    Lapse rate to next level down  K m   Distance to the next level down  m   Height of current level  m     SNT contains data relating to work produced when a parcel from the base level is raised true   adiabatically to the current level     Pit TS    Pressure  kPa    True adiabatic expansion temperature  K    Potential energy of condensed water  J kg air    Total mechanical energy  WB    Kinetic energy  WK WB WPP      SNP contains data relating to work produced when a parcel from the base level is raised  pseudo adiabatically to the current level     pa    Pressure  KPA    Pseudo Adiabatic expansion temperature  K    Water vapour content  g kg    Entropy of parcel excluding condensed water  J kg K     26    5  Water condensed in current expansion step  g kg    6  Accumulated potential energy of condensed water  WP    7 Enthalpy of condensed water   8  Enthalpy of vapour phase   9 Height z   10  Work of buoyancy AWB in current step   11  Cummulative work of buoyancy WB   12 Work of buoyancy minus potential energy of concensed water  WK WB WP     AT5A_ADIABATIC EXPANSION TEMPERATURES       The condition of the air to be expanded is stored in Matrix Beta and moved to the stack with  Beta GET  GTA generates the adiabatic expansion temperatures for 6 types of expansion and  puts the result in a seven column array  The array ends up o
23. air but limits the number of  properties that can be specified to two for saturated air  When the air is dry the third property is  zero  When the air is saturated  the third property is used to determine the quantity of  condensed water  The program checks if MM is beyond the saturation amount  if so the water  beyond the saturated amount is taken to be all in the liquid phase if the temperature is above  freezing temperature TF  or to be all in the ice phase if the temperature is below freezing  temperature TF minus the freezing band FB  The calculations are based on the air and the  water in any phase being at equilibrium  The calculated properties include the contribution of  the condensed water  Air masses can have water in two condensed phases     Once the required two or three properties are known all other thermodynamic properties of the  air mass are readily calculated     Example of program structure     Visiting U3 shows that P  T  M must be on the stack to calculate relative humidity and that the  program MVS is used in calculating the saturation mixing ratio    Visiting MVS  in AT3  shows that pressure and temperature must be on the stack to calculate  saturation mixing ratio and that the program PV is used in calculating the vapour pressure   Visiting PV shows temperature must be on the stack to calculate vapour pressure and that the  program PVL or PVI are used to calculate vapour pressure depending on whether the  temperature is above or below the freeze point
24. array  Pressure array with 5 kPa intervals    Generate sounding temperatures true adiabatic expansion  Generate sounding temperatures pseudo adiabatic expansion    Calculates the height of any pressure from the SNZ data   Calculates the virtual temperature at any pressure from the SNZ data     Calculates work produced when a parcel is lifted from h1 h2 mv z   Calculates potential energy of condensed water from m1 mv z   Moist static energy equation   Solve moist static energy equation for temperature    Average sounding entropy    Total and Average sounding enthalpy  Total and Average sounding water  mm H20     25    ZZ4 to ZZ8  WT1 to WT5  PD2 to PD9    Results array reversible no separation  true adiabatic     constant entropy   Results array irreversible no separation  constant static energy    Results array reversible with separation  Pseudo adiabatic     constant entropy   Results array reversible with separation  constant static energy    Copy result arrays SNT and SNP in SNTs and SNPs   Copy result arrays SNT and SNP in SNTo and SNPo    Generate parcel properties parcel properties in PCU format   Generate parcel properties parcel properties in PKM format   Generate parcel properties relative to sounding base enter AT and AM  Parcel Presure   Parcel Temperature   Parcel mixing ratio   Parcel entropy   Parcel enthalpy    Subsoutines used in calculating SNZ  Subroutines used in calculating SNT  Subroutines used in calculating SNP    SNZ contains the following sounding dat
25. ber for   free convection of air in a tube     enter  Delta T  mean T   Diameter    Calculations   Calculate all output data from input data  Calculate  Delta pressure for turbulent flow  Calculate  Delta pressure for laminar flow  Calculate  Delta pressure using friction factor F5  Calculate  Work loss per unit mass turbulent flow  Calculate  Work loss per unit mass laminar flow  Calculate  Reynolds Number   Calculate  Friction factor turbulent flow  Calculate  Friction factor laminar flow   Calculate  Tube cross sectional area   Calculate  Volumetric flow   Calculate  Mass flow   Calculate  Total work loss turbulent flow  Calculate  Total work loss laminar flow  Calculate  Ideal work from T  delta T  Z5     adiabatic lapse rate  Calculate  Ideal delta P from PCE    Input Data  Tube diameter    Velocity  Tube length    33    u5 Fluid viscosity  p5 Fluid density  F5 Friction factor    Output data    PT6 Pressure drop turbulent flow   PL6 Pressure drop laminar flow   WT6 Work loss per unit mass turbulent flow  WL6 Work loss per unit mass laminar flow  FT6 Friction factor turbulent flow   FL6 Friction factor laminar flow   FR6 Ratio of Turbulent to Laminar friction factors  Re6 Reynolds Number   A6 Tube area   QV6 Volumetric flow   QM6 Mass flow   TWT6 Total work loss turbulent flow   TWL6 Total work loss laminar flow   AT5F Properties with unit    AT5F contains one program called PROP  PROP calculates the properties of the air specified  in AT4 and tags each property with a na
26. c   The freezing temperature and the freezing bands  are 0  C and 20  C by default but can be changed     AT5J can calculate the maximum intensity  MPI  of hurricanes and the work produced in an  atmospheric Vortex Engine  AVE  work based on ideal process including a heater humidifier     AT5J calculation prerequisites include entering the properties of ambient air at state 1 using  either PCM1 or PCU1  entering the upper level pressure and level with PZ4     PCM1 Enter surface air conditions in PCM format   PCU1 Enter surface air conditions in PCU format   PJ4 Enter pressure   gt  Jordan Caribbean sounding hurricane height from lookup table  PJ4S Enter pressure   gt  Jordan Caribbean sounding hurricane height by interpolation  P4 Upper level pressure   Z4 upper level elevation   R1 Recall state 1 conditions in PCM format    Several of the objects use the two guesses method wherein the user enters one guess and   the program provides a second guess and then extrapolates to find the solution  Program using  the two guess method are identified with a    2    in their names  Results show the extrapolated  value and the residual error  The two guess programs can be rerun to reduce the residual error     Convection Energy wirhout heater humidifier  The following four CE  Convection Energy  programs are for a three states process where there    is no heater humidifier  Results are stored in parameters X1  X3 and X4  There is no state 2   The calculation can usually be carried out d
27. d then pressing the key for the desired property  The ending digit 3 in the program  name is used to indicate properties calculated from the three standard parameters     R Recall PP  TT  and MM to stack  TT in   K     PKM format   C Recall PP  TT  and MM to stack  Display in   C     PCM format     MOOXK  lt      gt  Ww    A1  PV3    UP3  UIS    MS3  MV3  ML3  MI3  p3    pD3  pL3  TV3    TV3S  ST3  SM3  SE3    AA3    HT3  HM3  EE3    HW4    u3  uAL3  T   9  0    gt T  63D  63M    Oe  e3  oWw3     L3    Toggle temperature in level 2 from   C to K   Recall PP  TT  and MM to stack  Display in   C     PCU format    Convert 3 stack properties from PKM format to PCU format   Convert 3 stack properties from PCU format to PKM format   Equivalent temperature air expanded to 10 kPa and compressed 100 kPa  isentropically    Backup PP  TT  MM in PPP  TTT  MMM    Store PP  TT  MM  in PPP  TTT  MMM  Calculate and store SS    Recall PPP  TTT  MMM to the stack     Vapour pressure  kPa    Relative humidity from mass ratio     saturation value relative to water      Relative humidity from partial pressure ratio       Relative humidity from mass ratio     saturation value relative to ice       Mixing ratio at saturation  g kg    Mixing ratio of water in the vapour phase  g kg    Mixing ratio of water in the liquid phase  g kg    Mixing ratio of water in the ice phase  g kg    Density  kg m3   Valid for moist air and for saturated air containing condensed  water    Density  kg m3   Moist air onl
28. diabatic expansion work   RPLT True adiabatic expansion work   SPLT Sounding Temperature Entropy Diagram   WPLT Virtual Temperature Excess of the parcel   TPLT Sounding Pressure Entropy Plot   XPLT Potential and Equivalent Potential Temperatures  YPLT Virtual and Potential Virtual Temperatures   ZPLT Double Potential Temperature    AT6A_Plot using HP48 parametric plot     AT6B plots equations based on the data in arrays  The result of the equation must be a  complex number  the real part is plotted on the horizontal axis and the complex part is plotted  on the vertical axis  The complex number may be taken directly from arrays or calculated from  array data  Plot is more flexible than MLINE  the X and Y can come from different arrays  the  data plotted not need to be in an array  it can be calculated from data in arrays  You can invoke  the plotter  edit the equation and add more line to a plot  Parametric plot is slower than MLINE   MLINE takes 10 seconds to plot a single line  Parametric plot can take 1 minute to plot a line  from an array without any calculation  calculating and plotting a property can take 5 minutes     The plots can be exported to a PC and printed with Word Perfect     45    1     REFERENCES    Dufour  L   et J  Van Mieghem  1975  Thermodynamique de l Atmosphere  Institut Royal  Meteorologique de Belgique  Bruxelles     Randall  D A   J  Wang  1992  The moist available energy of a conditionally unstable  atmosphere  J  Atmos  Sci   49  240 255     Ooyama
29. e HP48SX  The calculations were  independently checked on an equivalent MathCad program and on chemical engineering  process simulator PROII     HP48SX programs are called objects  Calculator programs are difficult to document and  therefore are rarely shared  The labelled programmable key features of the HP48SxX facilitate  the use of the calculator  The directories and the programmable keys of the directory are  organized to help one remember the name of function and sequence of use  The programs can  be viewed using the VISIT key as a supplements to this documentation  Objects are usually  kept short to make it easier to understand the programs  Parameters required to run a program  are usually listed at the beginning of the program code  RPN and algebraic programming mode  are both used  The algebraic mode is used to show equations their familiar form  Using the  HP48SX calculator requires an understanding of its two volumes User Manual  Using the  search function of your file reader can be an effective way of finding the topic or the object you  are looking for in this program documentation     The AT program can be modified to test scenarios not anticipated when the program was  conceived  The program and its documentation are a work in progress  The purpose of  infrequently used old objects may no longer be clear to the author  An attempt has been made  to remove unused and duplicate objects  Some of the objects whose usefulness is in doubt or  that may be used by othe
30. e Stefan Boltzman law  and earth surface area     Source  Earth s Annual Global Mean Energy Budget  J  T  Kiehl and Kevin E  Trenberth   Bulletin of the American Meteorological Society  Volume 78  Issue 2  February 1997   pp  197 208     Units are in W m        SCON Solar constant  342 W m       STR Solar radiation reflected by atmosphere and earth   s surface  107   SAR Solar radiation reflected by air and clouds  77   SGR Solar radiation reflected by ground  30    SAB Solar radiation absorbed by air and clouds  67   SGB Solar radiation absorbed by ground  168    IGE Infrared emitted by the earth   s surface  390   IGB Infrared absorbed by the earth   s surface  324   IGN Infrared net from the earth   s surface  66    CVT Convection from then earth   s surface  102   LGC Latent from ground  78    HGE Sensible from ground  24    IRT Infrared total  235    IGU Infrared upward from the earth   s surface  40   ICU Infrared upward from cloud  30    IAU Infrared upward from air  165     W  gt P Watts to percent  P  gt W Percent to Watt    SBC Stefan Boltzman constant  WR Radiative flux from temperature  TR Temperature from Watts    ESUR Earth   s surface  ERAD Earth radius  km   R A Radius  km  to area  km        FDO Forcing as a result of doubling CO  concentration  4 W m    FBB Forcing for Black Body  0 3   C  W m       FHA Forcing including all feedback from James Hansen  0 75   C  W m        AT3C_ THERMODYNAMIC PROPERTIES OF PROPANE   pV Density of propane gas in kg m3     ent
31. e updraft   Work calculated Using Michaud enthalpy     reversible updraft of given temperature and  RH   Work calculated Using Michaud enthalpy     irreversible updraft    Miscellaneous AT5J objects    SAB    T2C  EXT    SST  AAP  BAP    Enter Sea surface temperature  SST   temperature approach  AAP   and humidity  approach  BAP   Store in SST  AAP and BAP  This is an alternate to PZ4   Calculate temperature T2 and net work   Store W12 and Q23    Interpolate using work for two P3 guesses to determine P3 which makes W34 0    Sea surface temperature in   C   Air temperature approach to SST in   C   Air humidity approach to 100  in       PCaP Z4 calculation based on P1  T1     C  and lapse rate a     C m  and P4  Results are    stored in P4 and Z4     PCa Z Z4 calculation based on P1  T1     C  and lapse rate a     C m  and Z4  Results are    PS4  PW4  PE4  W95    HM    HMO    T4  T4E  BUO    stored in P4 and Z4    Enter pressure   gt  Standard atmosphere height    Enter pressure   gt  Standard winter atmosphere height   enter pressure   gt  Standard equatorial atmosphere height  Work calculation based on 95  RH  Enter SST    Michaud enthalpy     Enthalpy of air producing zero work  66900 J kg when air is raised  to Jordan 12 kPa level  15500m      Michaud enthalpy     Enthalpy of air producing zero work  59500 J kg when dry air is  raised to Jordan 12 kPa level  15500m      Temperature of parcel at level 4  Temperature of parcel at level 4  from P4JS   Buoyancy of parcel at lev
32. e values can be changed by the  user  For the default values  condensed water is all liquid temperatures above 0  C  all ice at  temperatures under  20  C  and 50  liquid at  10  C  Objects MV3  ML3  and MI3 in AT4 can be  used to calculate how much of the water is in each of the three phases     A freezing band is equivalent to the transition phase suggested by Ooyama both approaches  eliminates a singularity solver problem when all the condensate freezes suddenly  If the  condensate were to all to freeze suddenly during adiabatic expansion the air temperature would  rise and some of the condensate would have to re evaporate to conserve entropy  The freezing  band can be removed by setting FB to zero  Using a freezing band is preferable to using  sudden freezing even if the point where freezing starts or end is not known  A freezing band of  5 K is sufficient to eliminate the solver singularity problems  The program assumes that water in  the vapour phase is in equilibrium with liquid water if the temperature is above the bottom of the  freezing band and in equilibrium with ice otherwise     AT2 DIRECTORY   TAT4 Make sub directory AT4 the current directory   Directory AT2 contains constants    Z Converts degK to degC and vice versa  formerly named KC   If the number on  the stack is less than 150  TO  273 15  is added  if the number on the stack is    greater than 150 TO is subtracted  Pressing KC repeatedly toggles between  degK and degC     14    TO Temperature base  273 1
33. eat of fusion at TO   LSQ Latent heat of sublimation at the triple point of water  MW Molecular weight of water   G Acceleration of gravity  9 8 m s    GM Accelleration of gravity 9 80665 m s    D Dry adiabatic lapse rate  G CPV        RA RV   K Kilo  One thousand  1000    15    PO    PVO  PQ    PU  PW1  PW2  PE2    TS    TW1  TE1  TE2    KAIR    aAIR  aW  pAIR  VAIR  HVC  HVL    Base pressure for air  100 kPa   Standard pressure 101 325 kPa   Base pressure for water vapour  0 61070 kPa  Triple point pressure  0 61114 kPa    Standard atmosphere tropopause  11 000 m  pressure  22 65kPa   Winter standard atmosphere tropopause  8000 m  pressure  77 37 KPA   Winter standard atmosphere pressure  2000 m   32 29 kPA    Equatorial standard atmosphere tropopause  15 000 m  pressure  12 95 kPA     Standard atmosphere bottom temperature  288 15 K    Standard atmosphere top temperature  216 65 K    Standard Winter atmosphere bottom temperature  253 15 K   Equatorial standard atmosphere bottom temperature  301 15 K   Equatorial standard atmosphere top temperature  203 15 K     Standard Atmosphere Lapse Rate  0 00650 K m   Winter Atmosphere lapse rate  0 00608 K m   Equatorial Atmosphere lapse rate  0 00653 K m     Elevation of the top of the Standard Troposphere  11 000 m   Winter Atmosphere height  2000 m    Winter Atmosphere height  8000 m    Equatorial Atmosphere height  15000 m     Clapeyron equation coefficient for saturation with respect to liquid water  Clapeyron equation coefficie
34. efficient   CK Heat transfer coefficient   RO Outer radius  km    FK Coriolis factor   UC Central relative humidity   DEMA DeMaria  1994  hurricane velocity correlation     enter SST in   C    AT5M_ _ SOLAR CHIMNEY    ATMC  ATT    VT    Q down     CHI   VOR  LOR  ZDD    P1T7T    FNN    MU    Solar chimney cases     see list of case at ene of this section   Enter chimney base delta  AT   Calculate ideal work per unit mass  J kg     Ex  Manzanares   17  C   gt  109 91 J kg   Enter upward velocity  V  at the base of chimney  calculate power    Ex  Manzanares 8 m s   gt  power ideal 75147 W  actual power 41802 W  Exit  losses 21879 W  Friction losses 3952 W  Turbine losses 7514 W    Ex  Manzanares  8   Calculate heat input from chimney flow and from collector area    Chimney mode power calculation  Vortex mode power calculation  Friction loss increased by a factor of 5000  per Lorenz     Enter chimney height  Z   chimney diameter  and collector diameter   Ex  Manzanares  200  10  244    Enter chimney base pressure  P1   default 100 kPa   base ambient  temperature in   C and lapse rate  T   default 0 00975   C m stored in variable  D     EX  Manzanares  100  30  0 00975    Enter Insolation heat flux  F   collector efficiency  N  in percent  and turbine  efficiency in percent  Calculate total heat received and collector delta T  Ex  Manzanares 10800 W m2  31    80     Calculated upward mass flow of air in kg s    41    VUD      DDD Calculate turbine loss  WT  and display QQo  WI  W
35. el 4 with condensed water in and out     Extrapolation subroutine EXT variables    37    PY P3 for guess 1  WY Work 34 for guess 1  PZ P3 for guess 2  WZ Work 34 for guess 2    Work and heat calculated in T2C and used in WA2 and WD2  W12 Work of expansion process 12 for CE1R    Q01 Heat input required to reach state 1 assuming that the water is initially in the condensed  state and that the air and water are initially at temperature    tO     Enter    tO    the temperature  of air and water in   C  typically 20   C   This is a good representation of the heat input for  deep atmospheric cycle wherein essentially all the water separates from the air   Relevant to CE1R    Q03 Heat input required to reach state 3 assuming that the water is initially in the condensed  state and that the air and water are initially at temperature    tO     Enter    tO    the temperature  of air and water in   C  typically 20   C   This is a good representation of the heat input for  deep atmospheric cycle wherein essentially all the water separates from the air and  where in the air is subsequently sprayed with sea water     Q23 Heat received in process 23 for reversible expansion  CE1R   Q13I Heat received in process 23 for irreversible expansion  CE11     Work calculated in CE1R   WB Work of buoyancy     Convective Energy  CE corresponds to CAPE    MV Maximum velocity from WB   WP Potential energy of condensed water for true adiabatic expansion   WPP Potential energy of condensed water for pseudo
36. er P in kPa and T in K  PC Vapor pressure of propane in kPa     Enter T in K   RC Propane gas constant   188 7    22    HC Propane heat of combustion   50 292 000 J kg  LVO Propane heat of vaporization     430 310 J kg  MW Propane molecular weight    CW Propane liquid sensible heat   CP Propane gas specific heat at constant pressure  pL Propane liquid density     510 kg m3   aC Propane vapour pressure equation coefficient  6C Propane vapour pressure equation coefficient  yC Propane vapour pressure equation coefficient    AT3D CIRCULATION PRODUCED FROM THE EARTH S ROTATION       R1 Enter annulus radius to initiate calculation     V1 Enter annulus velocity for storage in V1   R1 Result annulus radius   V1 Result annulus velocity   R2 Result radial distance where C2   C1   V2 Tangential velocity at radius where C2   C1  C1 Circulation  C1   R1   V1   R2   V2   RAT Radius and velocity ration RAT   V2 V1  R2 R1  a1 vorticity at radius 1    1S__ vorticity at radius 1 solid body rotation    2 vorticity at radius 2     2S vorticity at radius 2 solid body rotation   FQ Coriolis factor from latitude    MOM Angular momentum     absolute   MOMR Angular momentum   relative to earth surface  MOME Angular momentum     earth surface   POTR Potential Radius     Emanuel  1999     AT3E LAMBTON COLLEGE PROTOTYPE PARAMETERS    AA8 Area of central 8    diameter hot air inlet     0 0324 m     A24 Area of central 24    diameter circle     0 29 m    AAS1 Area of one 6    x 48    deflector slot     0 
37. er kg of air    Calculates to quantity of water that must be mixed with air mass 1 to produce  saturated air of relative humidity U at temperature T with water at temperature  W    Enter air mass 1 properties using PCU1 or PCM1 prior to running WTUW   Tthe temperature of the liquid water in the mixture is the wet bulb temperature of  the air mixture  Enter    W the temperature of the water    T the temperature of the mixture    U the relative humidity of the mixture    P3 the pressure of the mixture    The mixture is assumed to be at pressure P3  M1 air is expanded isentropically  to from P1 to P3 prior to mixing    Result in mass of water MM2 in grams of water per kg air     Enthalpy check after running WTUW   no parameters required just press HCK  Results consist of four numbers    Enthalpy of gas phase in final state   Enthalpy of liquid phase in final state   Enthalpy of gas phase in initial state   Enthalpy of liquid phase in final state  Total enthalpy in the final state equals total enthalpy in the initial state     Entropy check after running WTUW   no parameters required just press SCK  entered   Results consist of four numbers    Entropy of gas phase in final state   Entropy of liquid phase in final state   Entropy of gas phase in initial state   Entropy of liquid phase in final state  Total entropy in the final state is greater than total entropy in the initial state  because internally generated entropy is generated during the irreversible mixing  process     29  
38. ers    Subsidence velocity required to compensate for radiative cooling   Carnot efficiency and ultimate efficiency  Efficiency of aimple and combined cycles     Tables of adiabatic temperatures for both true and pseudo adiabatic  expansion  the freezing temperatures is adjustable    Properties of isenthalpically mixed air and water    Data for the four cases described in   Thermodynamic Cycle of the Atmospheric  process       Case 1  air column with an adiabatic lapse rate  pure air    Case 2  air column with a 6 5 K km lapse rate  pure air    Case 3 and 4  air column with a 6 5 K km lapse rate  moist parcel    Properties of air rising with entrainment and detrainment  Used for Tellus paper   currently broken             Marqules type air masses change of position     AT5D    AT5E    ATE1    AT5F  AT5G  AT5H  AT5J  AT5J1  AT5J2  AT5J3  AT5K  AT5L  AT5M  AT5N    AT5P  AT5Q    AT6A  AT6B  AT6C  AT6D  AT6E    Independent check of adiabatic expansion temperature using a standard  equation for the entropy of moist air during adiabatic expansion  not used      Pressure drop and work loss for continuous flow in a tube   Drag  terminal velocity and work loss for spherical air parcels   Air to sea heat transfer     Tube flow calculations with stored data     Thermodynamic properties with tags  symbol and units   HP48 differentiation function test  unused     CAPE from sounding data    Hurricane intensity   AVE Ideal process     Total energy equation  Sarnia constants   Emperical ener
39. erves   WGR World gas reserves   WCR World coal reserves   WUR World uranium reserves   AT2B Car mileage conversions   GALC Toggle between Litres per 100 km to miles per Canadian gallon  GALU Toggle between Litres per 100 km to miles per US gallon  KPM Toggle between Litres per 100 km and kilometres per Litre  AT2C Energy price  Values based on September 2013 EIA    GJE Electricity per Giga Joule   33 33     JE Electricity per Joule   33 33E 9     KE Electricity per kilowatt hour   used to calculate others   0 12    GJO Crude oil per Giga Joule   15 5     JO Crude oil per Joule   15 5E 9     MTO Crude oil per metric ton   650     BO Crude oil per Barrel   used to calculate others   95    GJG Natural gas per Giga Joule   5 29      JG Natural Gas oil per Joule   5 29E 9     17     MG Natural gas per standard cubic meter   0 203    TFG Natural gas per standard thousand cubic feet   used to calculate  others   5 74      GJC Coal per Giga Joule   1 74     JC Coal per Joule   1 74E 9     MTC Coal per metric ton   45 10     TC Coal per US ton   used to calculate others   41 00    GJZ Gasoline per Giga Joule   26 5     JZ Gasoline per Joule   26 5E 9     LZ Gasoline per litre   0 92     GZ Gasoline per US gallon   used to calculate others   3 50   AT2D Hurricane categories minimum velocity in m s  VTS Tropical storm   VH1 Category 1 hurricane   VH2 Category 2 hurricane   VH3 Category 3 hurricane   VH4 Category 4 hurricane   VH5 Category 5 hurricane   KPH Convert m s to km hr   MPH Co
40. gy equations   Hurricane  amp  AVE total work   Exergy   Hurricane intensity   Emanuel method   Solar chimney   Pseudoadiabatic expansion temperatures       Equivalent Potential temperatures by step and by Bolton    Sounding arrays and array conversion programs  AT5J with addition of WK WB WPP   recognises that WP reduces WB     Plots array data using the HP48 parametric plot rather than MLINE   Sounding CAPE    Subsidence    Average properties of a sounding         AT4 PROGRAMS DESCRIPTION    Directory AT4 is described first because it is the most important and most frequently used  directory  Pressing ATM  in the HOME directory makes AT4 the current directory  AT4 makes  use of the constants in AT2 and of the pure air properties of AT3     Air properties can be entered in many ways     PKM Pressure in kPa  dry bulb in K  and mixing ratio in g kg    PKU Pressure in kPa  dry bulb in K  and relative humidity in      PCD Pressure in kPa  dry bulb and dew point in degC with respect to liquid water   PCM Pressure in kPa  dry bulb in C  and mixing ratio in g kg    PCU Pressure in kPa  dry bulb in degC and RH in      PCW Pressure in kPa  dry and wet bulb in degC    PCDF Pressure in kPa  dry bulb and dew point in degC with respect to ice    POM Pressure in kPa  potential temperature in K  and mixing ratio in g kg dry air   POQ Pressure in kPa  potential temperature in K  and humidity in g kg substance     To specify the air property  put the appropriate three properties on the stack
41. il   Joules per cubic meter natural gas  Joules per ton of crude oil   Joules per barrel of oil   Joules per ton of coal   Joules per tonne of TNT   Ton of oil per barrel    Time Conversion Factors    Seconds per day  Seconds per sidereal day  Minutes per day   Hours per year   Seconds per year    Miscellaneous Utilities    TICK  DONE  MLINE  GRAPHER  AUTHOR  SYMB    Short audible    Long audible    Plotting program    A program to transform an array to a string for transfer to a PC   Program author name   Calculator keyboard index    13    AT1 Custom Menu    The converts between SI and traditional units and works like the calculator   s built in unit  converter  To use the converter enter the value and press the key for the old unit  To convert to  an other unit press the left shift key and the key for the new unit  Press UVAL to remove the  unit tag     The AT1 custom menu has the following user defined keys  Conversion only works within a  category     Category UVAL   Energy Units J KW H BTU   Power Units W BTU H   Temperature Units C K F R  Volumetric flow L S GPM   Density KG M    LB FT     Energy Density G GJ T GW h    AT2 _ _ FREEZING BAND    Condensed water can freeze between 0  C K and  40  C  Condensed water can be made to  freeze over a band of temperature  FB  starting at a specified freezing temperature  TF    Freezing temperature TF and freezing band FB are stored in directory AT2  Default freezing  temperature is 273 15 K  default freezing band is 20 K but thes
42. irectly without any guess indicated by the    1    in the  program name or by providing one guess indicated by    2    in the program name     R    stands for  reversible expansion and    I    stands for irreversible expansion  There is no separation of the  condensate in either case     Convective Energy reversible process  CE1R Calculate the work produced when surface air is raised reversibly  Results shown are    T4  P3  thetaE and WB   Calculates P3 and T3  only valid if there is no condensation at  state 3      Convective Energy irreversible process Convective Energy reversible process  CE1  Calculate the work produced when surface air is semi reversibly  Enter turbine    efficiency  Results shown are T4  P3  and WB   Calculates P3 and T3  only valid if there  is no condensation at state 3    CE11 Calculate the work produced when surface air is raised irreversibly  Result T4  and P3   CER Subroutine used by CE2R   CE2R Calculate the work produced when surface air is raised reversibly  Enter a P3 guess     Results P3 and residual error  Can be rerun to reduce residual   minor bug run CE1R  first to correct     35    CE1R and CE2R results correspond to the CAPE of a true adiabatic updraft  When there is no  condensation at state 3 the two programs give the same result     CEI Subroutine used by CE2l     CE2I Calculate the work produced when surface air is raised irreversibly  Enter a P3 guess   Results P3 and residual error  Can be rerun to reduce residual     CE1I and CE2
43. l temperature of air with no  condensed water content  93M uses the solver to calculate the potential temperature of air  containing condensed water  Potential temperature can also be calculated using TSOL  TSOL  uses the solver to calculate the temperature at the end of an isentropic process  93D is much  faster than TSOL  but TSOL is more fundamental  entropy is conserved in isentropic processes   63M is valid for any kind of air including air containing condensed water  63D is only valid when  there is no water in a condensed phase  TSOL is valid for compression or expansion     The program makes extensive use of Gibb   s rule that states that knowing three properties is  sufficient to calculate all thermodynamic properties of a two component system  The three  properties need not be one of the set listed at the beginning of section 3 1  For example the  three properties can be  entropy  mixing ratio and pressure  TSOL calculates temperature from  entropy  mixing ratio and pressure  When TSOL is used it is only necessary to enter the  pressure  PP  because the values of entropy and the mixing ratio are taken from the calculator  memory  SS  MM   The high resolution of the HP48SX makes possible to reverse a calculation  to get back the originals input     AT4 Miscellaneous objects    SET Store stack in PP  TT  MM    IS Initialize by calculating entropy and storing it in SS    GF Accelleration of gravity factor of air water mixture   enter MM   KM Poisson ratio of air water 
44. lculate power  Calculates 01 and MU    CHI Work calculation     Press after VTDT  L osses based on turbulent flow  W    Based on AT5J WB in J kg  Results are  WR   WX  WF  and WT    VOR Work Calculation     Press after VTDT  Losses based on laminar flow  W    Based on AT5J WB in J kg  Results are  WR   WX  WF  and WT    DDD Calculate turbine loss  WT  and display WII  WAA  WX  WF  and WT   DVZp Friction loss calculation for turbulent and laminar flow  J kg   Enter  diameter  velocity   length and density    VCH Upward velocity at base of updraft  m s    DCH Diameter of updraft or solar chimney  m    pi Density of air at state 1  kg m    MU _Updraft flow  kg s    WR Reversible process work  W    WX Exit velocity losses  W    WF Friction losses  W    WT Turbine losses  W    EF Exit kinetic energy loss divider  Default 10    FF Laminar flow friction multiplier  Default 10    NT Turbine efficiency       Total work   WI Ideal work  W    WN Net work  W    WX Exit losses  W    WF Friction losses  W    WT Turbine losses  W     39    Specific work    wl Specific work     ideal reversible J kg    wX Specific work     Turbine loss  J kg    wF Specific work     Friction loss  J kg    wT Specific work     Turbine loss  J kg    wC Specific work     Work of compression  J kg   wE Specific work     Work of expansion  J kg     AT5K Energy calculations using Exergy    IRR Given p  t  m  pj  tj  and z  Calculates loss work    WEX6 Given p  t  m  pj  tj  and z  Calculates delta h  delta h     mg
45. lve H EQ for MM  Enter HH   MSOL Mixing ratio from wet bulb   Solve W EQ    PSOL Isentropic expansion pressure     Enter T   Solve S EQ for P given S  T and M   SSOL Isentropic expansion temperature     Enter P   Solve S EQ     Solve for T given S  P  and M     10    TCAL Isentropic expansion temperature     equation     no condensation allowed    TSOL Isentropic expansion temperature     Enter P     Invoke SSOL after calculating SS    Solve for T given S  P  and M    VSOL Temperature from Virtual temperature   Enter TV     Solve TV EQ   WSOL Wet bulb temperature   Solve W EQ     The following xxx 3 properties programs invoke the solver    TAS  0A3  TE3  0E3  663  LCL3  LFZ3  Properties calculated using the solver which require up  to a minute to calculate on the original HP48SX calculator can be calculated in under 1 second  on the emulator  The solver adds variables to the current directory  The use of the solver  should be restricted to the directories where the variables PP  TT  and MM exist  namely AT4   AT5  AT5B  AT5F  The solver can overwrite the values of PP  TT  MM  SS  and HH  Results  are always stored in the current directory  New variables appear at the front of the current  directory before the name of the first sub directory and can be purged once they are no longer  required  Programs B  Backup  and R  Restore  can be used to restore the standard properties  before the next calculations     63D calculates potential temperature using a formula for the potentia
46. me and unit  It is a quick way to check units used by  the program     12 2 AT5G  12 3  AT5H Upflow process calculations   WC Work Calculate     Enter P3 and Z3    HC Enthalpy calculate     Calculate air conditions at the base of the updraft in PCD format   Calculates P1  T1  and H1     ZC Height Calculate     Calculate Z1  the height of the P1 level  Used to calculate the  elevation at the base of a sounding when the station elevation is not provided     AT5J Hurricane intensity     Total Energy Equation method    AT5J contains objects for calculating work production when air is raised both reversibly and  irreversibly for a variety for conditions  Calculations are based on the total energy equation  method and on the four state ideal process shown in Fig 1 of the Isabel intensity paper   Calculation results at the four states are stored in variables  P1   P4  T1   T4  M1 M3  S1 S3   H1   H4  Other results include WB   work of buoyancy  WP   potential energy of condensed  water  Q   heat received  and maximum hurricane intensity in kPa and m s     The AT5J directory contains valuable programs  AT5J can be used to show that work is equal  to heat received times Carnot efficiency  AT5J can be used to calculate the final temperature of    34    air raised reversibly and irreversibly and to show that the final temperature is slightly higher for  irreversible upflow than for reversible upflow  All calculation are based on updraft without  separation  commonly called true adiabati
47. ments   Cloumns  PCTA  C  M  U  TV  entropy increase   Mixing result array    Calculates the property of a mixture of mass  1 and of the MM2 water part of  mass  2 where MM2 is in liquid state  TT2 and MM2 must be entered prior to  pressing TMW and are used to specify the temperature and quantity of  condensed water added to the humid air mass     Entropy of air water mixture    Calculates to quantity of water required to saturate mass 1 air at T by mixing with  water at temperature W  Enter the temperature of the water W and air mass 3  temperature T prior to pressing WTW     Calculates to quantity of water required to produce saturated air of relative  humidity U at T with water at temperature W   Water outlet temperature equal to  final air dry bulb temperature   Enter the temperature of the water W  air mass 3  temperature T and relative humidity U prior to pressing WTU     Calculates to quantity of water that must be mixed with air mass 1 to produce  saturated air of relative humidity U at temperature T with water at temperature    28    WTUP    HCK    SCK    W    Enter air mass 1 properties using PCU1 or PCM1 prior to running WTUW    The temperature of the liquid water in the mixture is the wet bulb temperature of  the air mixture  Enter    W the temperature of the water  T2     T the temperature of the mixture    U the relative humidity of the mixture    The mixture is assumed to be at pressure P1  there is no change in pressure   Result in mass of water MM2 in grams p
48. mixture     enter MM   RM Gas constant of air water mixture     enter MM   CPM Specific heat at constant pressure of air water mixture     enter MM  CST Custom menu    11    AT4 CUSTOM MENU  CST     The custom menu provides access to the most commonly used functions by using the A to F  keys in the unshifted  left shifted  and right shifted mode     KEY LABEL UNSHIFTED LEFT SHIFTED RIGHT SHIFTED  A RUM R PCU PCM   B SHp ST3 HT3 03   C SCF MS3 LCL3 LFZ3   D PUV PV3 U3 TV3   E Dwe DSOL WSOL TSOL   F KCF Z ZF ZC    There are two custom menus  CST  one in AT1 and one in AT4  The AT1 custom menu is  available in all subdirectory of AT1 down to AT4  The AT4 custom menu is available from all  subdirectory of AT4  The AT1 custom menu converts between non SI and SI units     The AT4 custom menu can be accessed from the AT1 directory with the TAT4 key and  pressing CST  The TAT4 key switches to directory AT4  Pressing SAT4 is a good way to get in  the program  it puts you in the middle of the program where the commonly used functions and  no more then two directories away     AT1 Conversion factors  times  and utilities        The purpose of the conversion factors is primarily to replace incoherent units into rational SI  unit  Energy units should be converted to the base energy SI unit  the Joules  Prefixes are not  used  Prefixes can be seen by going to engineering mode and looking at the exponent     Temperature Conversion    ZC Degree F to C   ZF Degree C to F   Power Conversion   
49. n the stack but is moved to AT6A  and called VT for plotting  The array columns are     Col Number Parameter   Pressure   True adiabatic freezing at 0 degC   True adiabatic freezing at  40 degC   True adiabatic no freezing   Pseudo adiabatic freezing at 0 degC   Pseudo adiabatic freezing at  10 degC   Pseudo adiabatic no freezing     NOOR WOD        GTA uses GT1  GT2  and GT3  GT1 produces the pressure column   GT2 produces true adiabatic expansion temperatures  GT3 produces pseudo adiabatic  expansion temperatures  GTA calculates expansion temperatures at 5 kPa pressure interval     PT Delta in AT6A plots the differences between the various adiabatic expansion temperatures  in VT  ET delta equation can be edited plot the difference between any two type of expansion   lines can be added to the plot     Programs TAT  TAP  and PAP list adiabatic expansion temperatures on the stack for a single  type of expansion     TAT True adiabatic at specified pressure interval   TAP Pseudo adiabatic at specified pressure interval   PAP Pseudo adiabatic at specified temperature interval     Sample arrays are stored in the program name preceded by a left arrow  PAP produces an  array that correspond to the Smithsonian Pseudo expansion tables  Theta WB calculates the  potential pseudo wet bulb temperature which is stored at the bottom of the array  The Potential  Pseudo wet bulb are in agreement with the Smithsonian tables  within 0 2 K     27    AT5B MIXTURE PROPERTIES    AT5B calculates the
50. nctions are  available     The name of the current directory and the path from the Home directory are indicated at the top  of the calculator screen  The name of the left hand key after you press VAR is the next directory  down  When you see the AT5 key you are in the AT4 directory     Sub directories  AT2  AT3  AT4  AT5  and AT6 form a chain    The objects in the upper level directories are available from any underlying directory  The  constants in AT2 are available in AT3  AT4  and AT5  the data in AT5 can be plotted in AT6   The objects not in in line directories are not accessible without changing directory  The  functions in AT4 can be accessed from AT5  AT5B can access the objects in AT4  AT3  and  AT2 but not the objects in AT5A  When the program encounters a new object  it looks for it first  in the current directory and then in its parent directories  The constant values are entered only  once  usually in AT2  therefore results are consistent and repeatable     Directory Structure    Parent Sub  Directories Directories  HOME AT1  AT1 AT2 AT2A AT2B AT2C AT2D ATDAT  AT2 AT3 AT3A AT3B ATSC ATSD  AT3E  AT3 AT4 AT4A AT4B AT4C  AT4 AT5 AT5A AT5B AT5C AT5D AT5E AT5F AT5G AT5H AT5J AT5K AT5L  AT5M AT5P  AT5Q  AT5 AT6 AT6A AT6B AT6C ATED AT6E  AT6 AT7    2 2 Main In Line directories   HOME Complete AT1 Program   Atmospheric Themodynamics Program AT1     AT1 Conversion between customary units and base SI unit  and energy content of  common fuels  Press ATM  to jump directly to
51. nt for saturation with respect to liquid water  Clapeyron equation coefficient for saturation with respect to liquid water    Clapeyron equation coefficient for saturation with respect to ice  Clapeyron equation coefficient for saturation with respect to ice  Clapeyron equation coefficient for saturation with respect to ice      User keys     No longer used  Coriolis Factor  2 n N     Viscosity of air   Viscosity of water   Prandt Number of air   Prandt Number of water  Conductivity of air   Conductivity of water   Diffusivity of air   Diffusivity of water   Density of air at standard conditions  Kinematic viscosity of air at standard conditions  Heating value of coal  J kg    Heating value of liquid fuel  J kg     16    AT2A Energy usage and reserves in Joules    All values are in Joules the base SI unit  Unit with SI prefixes can easily be inferred by going to  ENG mode     WPY World primary energy usage per year   WEY World electrical energy usage per year   WOY World oil energy usage per year   WGY World gas energy usage per year   WCY World coal energy usage per year   USEY US electrical energy usage per year   USOY US oil energy usage per year   USGY US gas energy usage per year   SUNS Solar radiation received by the earth per second   SUND Solar radiation received by the earth per day   SUNY Solar radiation received by the earth per year   HHS Hurricane thermal energy  heat  per second   HHD Hurricane thermal energy per day   WFR World fuel reserves   WOR World oil res
52. nter Carnot efficiency     from 7 terms of series    EFL Ultimate efficiency when work is dissipated at hot source temperature      Enter Carnot efficiency     from series ultimate limit   TH Default hot source temperature   TC Default cold source temperature   ATH Steam cycle hot source Delta T   ATC Steam cycle cold source Delta T    Q1 Q2  Q3   Q4 Heat input to each cycle and waste heat    Joule or Watt   W1  W2  W3  W123 Work from each cycle and total work _  Joule or Watt   A1  A2  A3 Actual efficiency to Carnot efficiency ratio     AT5 PROGRAM DESCRIPTION  AT5 contains programs to calculate properties for a whole sounding including how much work is    produced when a parcel is raised true adiabatically or pseudo adiabatically  Caution parcel  properties PP  TT  MM  SS etc    use in AT5 are not the same as used in AT4     aGET Gets the original sounding data in PKM format for the specified sounding level    BGET Gets the properties of pseudo adiabatic expanded air in PKM format for the  specified sounding level     GET Gets the properties of true adiabatic expanded air in PKM format for the  specified expansion level    pGET Get parcel properties    MIX Mixing calculator   63 Calculates the static energy per unit mass of air  ZB and SNZ are used to  calculate height    oM3 Calculates the static energy per unit mass of substance  ZB and SNZ are used    to calculate height     24    NW1    NW2    NW4    WPP    W1  W2    W4    SNC  SNK  SNZ  SNT  SNP    GSA  GSZ    So  PB  
53. nvert m s to mph   KT Convert m s to knot   VIA 76 m s   VIM 170 m s   EFO Enhanced Fujita category 0   EF1 Enhanced Fujita category 1   EF2 Enhanced Fujita category 2   EF3 Enhanced Fujita category 3   EF4 Enhanced Fujita category 4   EF5 Enhanced Fujita category 5   FUJ Old Fujita tornado class to m s   TOC Tropical Cyclone  135 m s     AT1 ATDAT Data directory   ATDAT contains data relating to specific soundings    STDA Standard atmosphere   EQUA Standard equatorial atmosphere   POLE Standard high latitude atmosphere   WILLIS Willis island sounding   JOR Jordan mean Caribbean hurricane season sounding  BRA1 Roscoe Braham pre lake Michigan sounding    FM3 Fawbush and Miller type  3 tornado sounding    GATE GATE sounding    18    HAW   Sounding    LEE Lee s convergence line sounding  LEMO LeMoyne sounding   LUCAS Lucas sounding   MK1 Makung pre severe squall sounding  PFLD Plainfield tornado sounding   RW Randal and Wang sounding   TEL TELLUS sounding     TRIER Trier sounding   WAT Watonga pre tornado sounding  WEI WEI sounding   WSPO   sounding   AEXP Expansion data generated in AT5A  PAP  TAT  TAP     The data directories can contains arrays of raw sounding data  SNC  SNK  SNU and arrays of  calculated data  SNZ  SNT  SNP  The arrays have the same names as the arrays of AT5   There are programs in AT4 to convert raw data arrays from one format to another  You can  store the SNC data in AT5 and recalculate the other arrays  or move all five arrays back to AT5   Program SAV 
54. o show that the result is the same as the  simpler ST3 program approach    SD2W Entropy of air containing water in the liquid phase    SD2l Entropy of air containing water in the ice phase    Four equations are required to calculate the adiabatic expansion temperature of rising air  one   for the moist air stage  one for the stage where the air contains water in the liquid phase  one   for the transition from liquid to ice  and one for the ice stage    The constant entropy approach used in AT4 is simpler  a single equation covers all four stages     AT5E TUBULAR AND SPHERICAL FLOW    Tubular flow   A5E1 TUBULAR FLOW USING STORED DATA  Input data identified with suffix    5     Output data identified with suffix    6      APF Pressure drop due to friction when fluid flows in a horizontal tube   From d  v  z  rho  f    APTA Frictional delta P for turbulent air  From d  v  z  rho    DPL Frictional delta P laminar air   APLA Frictional delta P for laminar air  From d  v  z  rho    APTW Frictional delta P turbulent water   APLW Frictional delta P laminar water   DVZW Delta P turbulent and laminar water flow   APW Calculate pressure reduction at the base of a vertical tube from pressure  the  temperature  and the work  p  k  w     APA Calculate pressure reduction at the base of a vertical tube from the work only   w   approximation    WF Work per unit mass loss through friction when a fluid flows in a horizontal tube     From d  v  z  f     31    DVZp  WLA    WTA    AREA  TVFL  TMF
55. or true  adiabatic expansion with water separation at the 10 kPa level    000    Equivalent Temperature using 003  enter PCU   00E3    Equivalent Temperature using 003  uses PP  TT  MM    HUX Canadian Humidex     Equation taken from Wikipedia   EMA3    Equivalent Temperature based on an equation from Emanuel  enter PKM   EMAU    Equivalent Temperature based on an equation from Emanuel  enter PKU   t4 Isentropic expansion temperature for moist air   not valid for saturated air    LCL3 Level of Condensation  kPa    LFZ3 Freezing pressure  kPa    Q3 Specific humidity  g kg    AFFK Affinity of air at PKM for liquid water at the temperature of the air   AFFC Affinity of air at PCU for liquid water at the temperature of the air   AC Affinity of pure water vapour at pressure FF for water at temperature  in   C    FF Vapor pressure in kPa  FF calculated by either AFFK or AFFC   Example     Arguments  1 90 2 293 15 3 12 00  Function  ST3   Result  212 47   Entropy is  212 47 J kg K    The program is valid for 3 kinds of air     1  Dry air where the moisture content is zero    2  Moist air where the moisture is less than the saturated amount    3  Saturated air where the water content is equal or greater than the saturation  amount     The three standard properties are used for the three kinds of air  Two properties are required  to describe dry air  three properties are required to describe moist or saturated air  The phase  rule allows three properties be specified to describe humid 
56. r objects have been retained  Questions marks are used for the  descriptions of objects that have not yet been documented     Calculated thermodynamic properties list    Partial Pressure of Water    Partial Pressure of Air    Mixing Ratio for Water in any Phase   Specific Humidity   Mole fraction of water   Relative Humidity    Wet Bulb Temperature    Density    Virtual Temperature    Potential Virtual Temperature    Entropy    Enthalpy    Free Enthalpy   Potential Temperature at 100 kPa    Double Potential Temperature  potential temperature at 10 kPa   Isentropic Desiccation Temperature   Potential Isentropic Desiccation Temperature  Equivalent Temperature  Isenthalpic Desiccation Temperature    Equivalent Potential Temperature   Lifting Condensation Pressure   Freezing Level   Level of Free Convection   True Adiabatic Expansion Temperatures   Pseudo Adiabatic Expansion Temperature   Potential pseudo wet bulb Temperature   Affinity    Static Energy     The calculations are based on Thermodynamique de I Atmosph  re by Louis Dufour and  Jacques Van Mieghem  Thermodynamic functions are generally based on the equations listed    in  http   vortexengine ca misc AT1_Equations pdf    The program uses rigorous definitions of thermodynamic properties and avoids algebraic  approximations  The HP48 solver is used to calculate properties that cannot be isolated by  algebraic manipulation rather than by using approximate equations  As a result running the  calculation backwards reproduce
57. recall the five arrays and their names to the stack  To move all arrays back to  the AT5 directory  recall SAV to the stack and press EVAL  switch to the AT5 directory  FM3   and press STO 5 times  The opposite procedure can be used to move the arrays from AT5 to  ATDAT  Arrow down AT5 changes to the AT5 directory     SEN     Arrays Summarizing the result of sensitivity analysis for the sounding  The  second  third  and fourth columns contain the potential energy of the condensed  water  the residual work  and the total work  The number in the first column is a  code indicating the type of expansion  the freezing temperature  the parcel  temperature excess  and the parcel mixing ratio excess   Column 1 code  1 true adiabatic expansion  2 pseudo adiabatic expansion  Column 2 code  0 freezing at 0 C  1 freezing at  10 C  4 freezing at  40 C  9 no freezing  Column 3 code  parcel temperature excess  K  beyond  base of sounding value  Column 4 code  parcel mixing ratio excess beyond base  of sounding value  g kg or 1 10 g kg     AT3 PROGRAM DESCRIPTION    Directory AT3 contains programs to calculate the thermodynamic properties of pure air and  pure water  the virtual temperature of moist air  lapse rate and distance between two sounding  levels     PV Partial pressure of water from T   PVL Partial pressure of liquid water from T   same as PGL   PVI Partial pressure of ice from T   same as PGI     19    PV2    MVS  MVL    pA    SA  SV  sL    SL3  SI    SC3    ZTA   ZPT   ZPTA  ZPT
58. s the original inputs     HP48 functions are written in algebraic notation so that the user can see the equations used to  calculate a property and the parameters required by the program by visiting the program   Calculator programs can be extremely useful but are notoriously difficult to document  For this  reason the use of calculator programs is frequently limited to the program creator  This  documentation is an attempt to explain the major features of the program  This documentation  is organized by directory  Object in directories are usually listed in the order they appear in the  calculator  A good way to find what you are looking for is to use your pdf reader search  function  The program and its documentation are works in progress     The program uses SI units  Directory AT1 contains objects for converting non SI units to the  base SI unit  Calculations are usually based on absolute temperature in degree Kelvin   Temperature can be entered in degree Celsius or Kelvin  Extensive properties are per unit  mass of dry air  Enthalpy of moist air is in Joules per kilogram of dry air and includes the  enthalpy of the air and its water content in any phase  Engineering multiples of the basic SI unit  are used when appropriate  pressure is in kPa  mixing ratio is in g water kg air  Units are not  shown except in directory AT5F  Program PROP in AT5F calculates 28 properties of the air  mass defined in AT4 and tag the values with the appropriate SI unit     The program can plo
59. t arrays of properties calculated from atmospheric soundings  The  program is designed so that the calculated properties can be used in subsequent calculations  including plots based on arrays of sounding properties  Entropy calculations were checked  against Randall  mixing calculations were checked against Lilly     2 0 PROGRAM INSTALLATION    The compete Atmospheric Thermodynamics program is contained in object AT1  The program  is installed by putting object AT1 on the stack and saving it as AT1 in the Home directory     AT1 requires 155 kbytes of memory  A real HP48SX calculator requires at least one 128 kbytes  memory card  This memory card must be merged in the built in 32 kBytes main memory to give  a total memory of 160 kbytes     An HP48SxX can have up to 290 kbytes of memory by merging two 128 kbytes memory card  with its basic 30 kbytes of memory  The HP48SX emulator should be set up with 290 kbytes of  memory     The AT1 program will run on either the HP48SX or the HP48GX or on their PC emulators  AT1  was written for the HP48SX  The HP48SX has a more consistent user interface than the  HP48GX and is recommended  On a PC  the use of the Casey touch screen HP48SxX skin is  recommended     2 1 DIRECTORY ORGANIZATION  Sub directory AT2 is accessed by pressing the AT1 key in the home directory     The left hand key in each directory is usually the next directory down  The TAT4 key in sub   directory AT2 gets one directly to the AT4 directory from which most of the fu
60. taking 10 minutes on the original  calculator can be completed in less than 2 seconds on a PC     HP48 emulators for IPod and IPad are now available for  15 at the Apple Application store  On  the IPod IPad emulators the key can be pressed directly like on the original calculators  In  addition the IPad emulator provides visual and audible feedback when key are pressed  resulting in a fabulous user interface  HP48 emulators are also available for Android devices     For some unexplained reason the skin for the PC version of the HP48SX calculator reversed  the color of the orange and blue shift keys  The skin for the HP48SX IPad emulator reverted to  the original colors which match those of the HP48SX Manual     The AT1 program can be run on the HP48SX or HP48GX original calculators  on windows  PC   s  on IPod  on IPad and on Android devices  AT1 requires 160 kBytes of memory  HP48SX  PC emulator memory can be increased from 30 kB to 292 kB by merging two 128 kB memory  cards  HP48GX PC emulator memory can be increased from 128 kB to 259 kB by merging one  128 kB memory card  The IPod IPad applications now support the second memory card and  therefore their maximum memory is 292 kB for the HP48SX app and 256 kB for the HP48GX    app     According to Vaclav Smil  a well programmed calculator is probably the most cost and time  effective investment an inquisitive mind can make in a life time  Calculations relating to the  Atmospheric Vortex Engine  AVE  can be carried out on th
61. thalpy of  large air masses   2  Programs to calculate the work produced when thin layer of dry air are    raised  including the efficiency of the process and the height of air  columns of uniform potential temperature     Calculate the height of a layer of air of uniform potential temperature   Enter P1  P2  and 9     Margules equation for the total enthalpy of large air masses from bottom  and top pressure  bottom temperature  and lapse rate     Margules equation for the total enthalpy of large air masses from bottom  and top pressure and potential temperature     Work produced when a thin layer of dry air is raised  from potential    30    temperature  parcel temperature  and height     WP Theta T Work produced when a thin layer of dry air is raised  from bottom and top  pressure  potential temperature  and parcel temperature     N Theta Z Efficiency from potential temperature and height    ZP Theta Height from bottom and top pressure and potential temperature    Subdirectory AT5C1 contains a program for calculating the area that two air equal air masses   of different potential temperature would require so that they have the same height  Invoke the   solver  enter Theta 1  Theta 2  and PT the pressure at the top of the air mass  Solve for height   ZZ  press A1 and P1 to obtain the area of air mass  1 and the pressure at the base of A1    10 0 AT5D contains the equation given by Dufour and also by Iribarne and Godson for the  entropy of humid air expanding isentropically t
62. tion from t     Height from T1 T2  and lapse rate    Height from P1  P2  T1  T2    Height from P1  P2  T1  and lapse rate    Height from P2 and T1  P1   100 kPa  Lapse rate adiabatic   P2 from P1  T1  in K   lapse rate  and height  solar chimney   P2 from P1  T1  in   C   lapse rate  and height  solar chimney   Temperature from P1  P2  T1  and lapse rate     Equation relating PX1  PX2  CX1  aX  ZX  Ambient Conduit bottom pressure  Ambient Conduit top pressure   Ambient bottom temperature     C   Ambient lapse rate  K km     20    ZX    a4  y4  yxa  axy  NXy  yXN  CNa  CNy    ZS  ZTS  AZS    ZTW  AZW    ZTE  AZE    NCC  NCK  MOL    R gt Q  Q    gt R    POP    POPA  POP1    OZPO  6ZOT    PGL  PGI  XVL  XVI     BV  tBV   TAU  ER    Ambient Conduit top pressure    Lapse rate from P1  P2  TV1  TV2   Poison exponent from P1  P2  TV1  TV2   Poison exponent from Lapse rate    Lapse rate from Poison ratio    N from Poison ratio   poison ratio rate from N   Specific heat from lapse rate   Specific heat from Poison ratio    Height in the Standard Atmosphere from P2    Height and temperature in the Standard Atmosphere from P2   Height difference in the Standard Atmosphere from P1 and P2   Height in the Winter Atmosphere from P2    Height and temperature in the Winter Atmosphere from p2   Height difference in the Winter Atmosphere from P1 and p2   Height in the Summer Atmosphere from p2    Height and temperature in the Summer Atmosphere from p2   Height difference in the Summer Atmosphere
63. to find datum relative humidity for which W   0    WUA2 Calculate relative humidity U3 required to make the work zero given C3 using two  guesses method  Provide relative humidity guess      OK for zero work   Needs fixing when work  gt  0     WPU2 Calculate temperature C3 required to produce pressure P3 at relative humidity RH3    WPU Calculate work for U3 given T3    PU Enter Pressure  P3  and relative humidity  RH3  in state 3 before running WPU or WPU    WPU2 Calculate T3 required to make the work zero given C3 using two guesses method   Provide one C3 guess     Note  The four W 2 solvers give result in y register error in x register  The error can be deleted    36    S97  S100  SSA  SSI  SSW    X1  X2    WM3  WM4    WM5    and W 2 can be pressed again to produce more accuracy  Results can be displayed in  more detail by deleting the results and pressing X1 or X2     Hurricane Maximum Potential Intensity  MPI  from SST     97  eyewall relative humidity   amp  with freezing   Hurricane Maximum Potential Intensity  MPI  from SST     100  eyewall relative humidity   amp  without freezing  PROII equivalent    Hurricane air temperature from SST      T3   24 5    SST    SSI    SSW   Hurricane Intercept  SST at which T3 24 5   C  default 27   C      used in SSA   SST Weighing  Delta T3   Delta SST  default 0 75      used in SSA    Hurricane Potential Intensity T3  WP  WB  WT  Hurricane Potential Intensity T3  P3  Pc  WB  v     Work calculated Using Michaud enthalpy     reversibl
64. y  Dufour and Van Mieghen equation 8 63   Density  kg m3   Moist air only  Leonard density of air plus density of water   Virtual temperature  K   Valid for moist air and for saturated air containing  condensed water    Virtual temperature of saturated air without condensed water  K    Entropy per unit mass of air  J kg K    Entropy per unit mass of substance  J kg K    Entropy from a common equation  equation possibly from Emanuel    Equivalent to ST3  Enter PKM    Entropy if water is in condensed phase   Enter PKM     Enthalpy per unit mass of air  J kg   Enthalpy per unit mass of substance  J kg   Enthalpy when water is in condensed state   Dufour Equivalent Temperature 12 39    Enthalpy at wet bulb temperature     Free enthalpy   H     TS   J kg    Free enthalpy     all water in liquid phase  J kg    Temperature to Potential Temperature   Potential temperature to Temperature   Potential Temperature of dry or unsaturated air   Potential Temperature of any air including air with condensed water  solver     Equivalent Temperature from Memory PTM  Equivalent Temperature from entered PTM  Wet bulb from entered PTM    Liquid water potential temperature    6V3 Virtual potential temperature  K       TA3 Isentropic Desiccation Temperature  K    6A3 Potential Isentropic Desiccation Temperature      Dufour 14 23   K    6E3 Equivalent Potential Temperature   TE3 Equivalent  Isenthalpic Desiccation  Temperature  K    003 Temperature at 10 kPa  K  and equivalent potential temperature f
65. z  exergy    WEXZ Given p  t  m  pj  and z  Calculates work from delta h  mgz    EXR5 Given p  t  m  pj  and tj  Calculates exergy    EXRZ Given p  t  m  pj  tj  and z  Calculates  delta h  tj delta s  ideal work    GIBB  gt Givenp t m  Calculates Gibb free energy    AT5L Hurricane Intensity     Renno   Emanuel equations    Renno Equation  A simple theory for Dust Devils 1998 eq  16     POC Calculate base pressure   PCUc Enter base pressure  temperature and humidity   Poa Far Environment Pressure   Ta Far environment Temperature   TO Central Temperature    C    To SST temperature    C    Mo Far Environment mixing ratio   Mas Far environment saturation mixing ratio   MO Central mixing ratio   Ua Far environment Relative Humidity   AN Efficiency multiplied by fractional dissipation in boundary layer  PCUA Enter surface condition in PCU format  Use SST for C    VK Maximum velocity     without frictional reheat   K Kerry   VKB Maximum velocity     with frictional reheat  KB  Kerry Bister     Bister and Emanuel  1998  eq   21   Emanuel  1999  eq   1   EK Efficiency without frictional reheat    40    EKB    Efficiency with frictional reheat    V86 Maximum velocity     Emanuel  1986  eq   43   VKD V86 denominator term   VKN V86 Numerator term   B86 V86 beta term   PC Central pressure     Emanuel  1986  eq   26   LPA  LPB  LPC  LPD PC terms   PE  TE  ME  MES  UE Surface conditions   HS Enthalpy of saturated air at SST   HE Enthalpy of surface air   TO Outflow temperature   CD Drag co
    
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