Cryogenic rocket calorimeter chamber experiments and heat transfer simulations

34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 1998, Pages

  Preclik, D ^a   Wiedmann, D ^a   Oechslein, W ^a   Kretschmer, J ^a  

^a AIRBUS GROUP INNOVATIONS   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

CALORIMETERS; COMPUTATIONAL FLUID DYNAMICS; COOLING; CRYOGENICS; ENGINES; HEAT FLUX; LIQUID PROPELLANTS; PROPULSION; ROCKET ENGINES; ROCKETS; SOFTWARE TESTING;

CHAMBER EXPERIMENTS; DROPLET SIZE DISTRIBUTIONS; GAS-PHASE COMBUSTION; HEAT TRANSFER SIMULATION; OPERATIONAL CONDITIONS; REALISTIC SIMULATION; REGENERATIVE COOLING; WALL HEAT TRANSFER;

HEAT TRANSFER;

EID: 79954563227     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (9)

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8. Gordon, S., and B. J. McBride, Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications”, NASA Lewis Research Center, NASA Reference Publication 1311, 1996.
9. Dunn, S. S., Coats, D. E., Nickerson, G. R., and D. R. Berker Two-Dimensional Kinetics Nozzle Performance Computer Program, Volume I, Engineering Methods”, Software and Engineering Associates, Inc., Carson City, Nevada, 1991.