NASA-GLENN CHEMICAL EQUILIBRIUM PROGRAM CEA2, FEBRUARY 5, 2004
                   BY  BONNIE MCBRIDE AND SANFORD GORDON
      REFS: NASA RP-1311, PART I, 1994 AND NASA RP-1311, PART II, 1996

 *******************************************************************************

  
 prob case=55312577 tp
   p(atm) = 20
   t,k=  3491.86
 reac
   name O2              wt%= 88.89
   name H2              wt%= 11.11
 output trace=1e-5
 only H  H2O  O  H2  O2  OH
 end

 OPTIONS: TP=T  HP=F  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

 T,K =  3491.8600

 TRACE= 1.00E-05  S/R= 0.000000E+00  H/R= 0.000000E+00  U/R= 0.000000E+00

 P,BAR =    20.265000

    REACTANT          WT.FRAC   (ENERGY/R),K   TEMP,K  DENSITY
        EXPLODED FORMULA
 N: O2               0.888900   0.000000E+00     0.00  0.0000
          O  2.00000
 N: H2               0.111100   0.000000E+00     0.00  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 6/97  *H               tpis78  *H2              g 8/89  H2O            
  g 5/97  *O               g 4/02  *OH              tpis89  *O2            

 O/F =   0.000000

                       EFFECTIVE FUEL     EFFECTIVE OXIDANT        MIXTURE
 ENTHALPY                  h(2)/R              h(1)/R               h0/R
 (KG-MOL)(K)/KG        0.00000000E+00      0.00000000E+00      0.00000000E+00

 KG-FORM.WT./KG             bi(2)               bi(1)               b0i
  *O                   0.55558333E-01      0.00000000E+00      0.55558333E-01
  *H                   0.11022481E+00      0.00000000E+00      0.11022481E+00

 POINT ITN      T            O           H 

               THERMODYNAMIC EQUILIBRIUM PROPERTIES AT ASSIGNED

                           TEMPERATURE AND PRESSURE

 CASE = 55312577       

             REACTANT                    WT FRACTION      ENERGY      TEMP
                                          (SEE NOTE)     KJ/KG-MOL      K  
 NAME        O2                           0.8889000         0.000      0.000
 NAME        H2                           0.1111000         0.000      0.000

 O/F=    0.00000  %FUEL=  0.000000  R,EQ.RATIO= 0.991974  PHI,EQ.RATIO= 0.000000

 THERMODYNAMIC PROPERTIES

 P, BAR            20.265
 T, K             3491.86
 RHO, KG/CU M    1.0852 0
 H, KJ/KG          4.8953
 U, KJ/KG        -1862.42
 G, KJ/KG        -57729.0
 S, KJ/(KG)(K)    16.5338

 M, (1/n)          15.548
 (dLV/dLP)t      -1.05733
 (dLV/dLT)p        2.0109
 Cp, KJ/(KG)(K)   12.8232
 GAMMAs            1.1252
 SON VEL,M/SEC     1449.5

 MOLE FRACTIONS

 *H              4.6666-2
 *H2             1.3094-1
 H2O             6.4610-1
 *O              2.1827-2
 *OH             1.1303-1
 *O2             4.1434-2

  * THERMODYNAMIC PROPERTIES FITTED TO 20000.K

    PRODUCTS WHICH WERE CONSIDERED BUT WHOSE MOLE FRACTIONS
    WERE LESS THAN 1.000000E-05 FOR ALL ASSIGNED CONDITIONS

 NOTE. WEIGHT FRACTION OF FUEL IN TOTAL FUELS AND OF OXIDANT IN TOTAL OXIDANTS