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         NASA-GLENN CHEMICAL EQUILIBRIUM PROGRAM CEA2, MAY 21, 2004
                   BY  BONNIE MCBRIDE AND SANFORD GORDON
      REFS: NASA RP-1311, PART I, 1994 AND NASA RP-1311, PART II, 1996

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 !     COMBUSTION OF HYDROGEN IN OXYGEN
 !     (a)  Combustion or assigned-enthalpy-and-pressure problem (hp).
 !     (b)  Fuels is  H2  at 298.15 K. The oxidant is O2 at 298K.
 !     (c)  Oxidant-to-fuel weight ratio is specified interms of phi=1
 !     (d)  Mixture enthalpy is calculated from reactant values given in
 !          thermo.lib. This is because data for these species are given in
 !          thermo.lib and the species names match exactly.
 !     (e)  product species considered is  H2O ('only' dataset)
 .
 !          Note:  these species names must match those used in thermo.lib.
 !     (f)  Assigned pressure is 1atm.
 !     (g)  Mixture properties are to be printed in SI units (siunits).
 !     (h)  Mole fractions > 1.e-15 are to be in e-format (trace=1.e-15).
 !
 reac
      oxid O2 moles=1 t(K)=298.15
      fuel H2 moles=1 t(K)=298.15
 prob
      case=Hydrogen_Oxygen   hp  p(atm)=1, phi=1
 only
      H2O
 output
      siunits  trace=1.e-15
 end  End all input for Hydrogen_Oxygen

 OPTIONS: TP=F  HP=T  SP=F  TV=F  UV=F  SV=F  DETN=F  SHOCK=F  REFL=F  INCD=F
 RKT=F  FROZ=F  EQL=F  IONS=F  SIUNIT=T  DEBUGF=F  SHKDBG=F  DETDBG=F  TRNSPT=F

 TRACE= 1.00E-15  S/R= 0.000000E+00  H/R= 0.000000E+00  U/R= 0.000000E+00

 P,BAR =     1.013250

    REACTANT           MOLES    (ENERGY/R),K   TEMP,K  DENSITY
        EXPLODED FORMULA
 O: O2               1.000000  -0.154035E-05   298.15  0.0000
          O  2.00000
 F: H2               1.000000  -0.326752E-06   298.15  0.0000
          H  2.00000

  SPECIES BEING CONSIDERED IN THIS SYSTEM
 (CONDENSED PHASE MAY HAVE NAME LISTED SEVERAL TIMES)
  LAST thermo.inp UPDATE:    9/09/04

  g 8/89  H2O            

 O/F =   7.936683

                       EFFECTIVE FUEL     EFFECTIVE OXIDANT        MIXTURE
 ENTHALPY                  h(2)/R              h(1)/R               h0/R
 (KG-MOL)(K)/KG       -0.16208918E-06     -0.48137850E-07     -0.60888815E-07

 KG-FORM.WT./KG             bi(2)               bi(1)               b0i
  O                    0.00000000E+00      0.62502344E-01      0.55508435E-01
  H                    0.99212255E+00      0.00000000E+00      0.11101687E+00

 POINT ITN      T            O           H 

 SINGULAR MATRIX, ITERATION  1  VARIABLE  2(EQLBRM)

 SINGULAR MATRIX, ITERATION  2  VARIABLE  2(EQLBRM)

 SINGULAR MATRIX, ITERATION  3  VARIABLE  2(EQLBRM)

 SINGULAR MATRIX, ITERATION  4  VARIABLE  2(EQLBRM)

 WARNING!! POINT  1 USES A REDUCED SET OF COMPONENTS
 SPECIES CONTAINING THE ELIMINATED COMPONENT ARE OMITTED.
 IT MAY BE NECESSARY TO RERUN WITH INSERTED CONDENSED SPECIES
 CONTAINING COMPONENT       H (EQLBRM)

 POINT ITN      T          H2O         
   1   10    4930.564     -38.028




         THERMODYNAMIC EQUILIBRIUM COMBUSTION PROPERTIES AT ASSIGNED

                                   PRESSURES

 CASE = Hydrogen_Oxygen

             REACTANT                       MOLES         ENERGY      TEMP
                                                         KJ/KG-MOL      K
 OXIDANT     O2                           1.0000000         0.000    298.150
 FUEL        H2                           1.0000000         0.000    298.150

 O/F=    7.93668  %FUEL= 11.189834  R,EQ.RATIO= 1.000000  PHI,EQ.RATIO= 1.000000

 THERMODYNAMIC PROPERTIES

 P, BAR            1.0132
 T, K             4930.56
 RHO, KG/CU M    4.4527-2
 H, KJ/KG         0.00000
 U, KJ/KG        -2275.58
 G, KJ/KG        -86535.6
 S, KJ/(KG)(K)    17.5509

 M, (1/n)          18.015
 (dLV/dLP)t      -1.00000
 (dLV/dLT)p        1.0000
 Cp, KJ/(KG)(K)    3.3823
 GAMMAs            1.1580
 SON VEL,M/SEC     1623.3

 MOLE FRACTIONS

 H2O             1.0000 0

  * THERMODYNAMIC PROPERTIES FITTED TO 20000.K

    PRODUCTS WHICH WERE CONSIDERED BUT WHOSE MOLE FRACTIONS
    WERE LESS THAN 1.000000E-15 FOR ALL ASSIGNED CONDITIONS