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=55312917 hp p(atm)=20 phi=1 reac fuel H2 wt%= 100.0 t,k= 350.00 oxid O2 wt%= 100.0 t,k= 350.00 output short output trace= 1e-5 only H H2O O H2 O2 OH end THERMODYNAMIC EQUILIBRIUM COMBUSTION PROPERTIES AT ASSIGNED PRESSURES CASE = 55312917 REACTANT WT FRACTION ENERGY TEMP (SEE NOTE) KJ/KG-MOL K FUEL H2 1.0000000 1502.518 350.000 OXIDANT O2 1.0000000 1531.068 350.000 O/F= 7.93668 %FUEL= 11.189834 R,EQ.RATIO= 1.000000 PHI,EQ.RATIO= 1.000000 THERMODYNAMIC PROPERTIES P, BAR 20.265 T, K 3501.57 RHO, KG/CU M 1.0744 0 H, KJ/KG 125.90 U, KJ/KG -1760.32 G, KJ/KG -58102.5 S, KJ/(KG)(K) 16.6292 M, (1/n) 15.435 (dLV/dLP)t -1.05843 (dLV/dLT)p 2.0267 Cp, KJ/(KG)(K) 13.0266 GAMMAs 1.1254 SON VEL,M/SEC 1457.0 MOLE FRACTIONS *H 4.8442-2 *H2 1.3501-1 H2O 6.4082-1 *O 2.2043-2 *OH 1.1345-1 *O2 4.0232-2 * THERMODYNAMIC PROPERTIES FITTED TO 20000.K NOTE. WEIGHT FRACTION OF FUEL IN TOTAL FUELS AND OF OXIDANT IN TOTAL OXIDANTS