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=44623075 hp p(atm)=20 phi=1 reac fuel H2 wt%= 100.0 t,k= 298.15 oxid O2 wt%= 100.0 t,k= 298.15 output short output trace= 1e-5 only H H2O O H2 O2 OH end THERMODYNAMIC EQUILIBRIUM COMBUSTION PROPERTIES AT ASSIGNED PRESSURES CASE = 44623075 REACTANT WT FRACTION ENERGY TEMP (SEE NOTE) KJ/KG-MOL K FUEL H2 1.0000000 0.000 298.150 OXIDANT O2 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 20.265 T, K 3491.86 RHO, KG/CU M 1.0804 0 H, KJ/KG 0.00000 U, KJ/KG -1875.66 G, KJ/KG -57941.0 S, KJ/(KG)(K) 16.5932 M, (1/n) 15.479 (dLV/dLP)t -1.05735 (dLV/dLT)p 2.0110 Cp, KJ/(KG)(K) 12.8800 GAMMAs 1.1253 SON VEL,M/SEC 1452.8 MOLE FRACTIONS *H 4.7123-2 *H2 1.3352-1 H2O 6.4615-1 *O 2.1406-2 *OH 1.1194-1 *O2 3.9854-2 * THERMODYNAMIC PROPERTIES FITTED TO 20000.K NOTE. WEIGHT FRACTION OF FUEL IN TOTAL FUELS AND OF OXIDANT IN TOTAL OXIDANTS