Numerical analysis of pulse detonation engines using global and reduced hydrocarbon kinetics

9th International Space Planes and Hypersonic Systems and Technologies Conference

Volumn , Issue , 1999, Pages

  Mawid, M A ^a   Park, T W ^a   Sekar, B ^b   Arana, C ^b  

^a Engineering Research and Analysis Company   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; CHEMICAL ANALYSIS; CHEMICAL REACTIONS; COMPUTATIONAL FLUID DYNAMICS; DETONATION; JET ENGINES; PROPANE; SENSITIVITY ANALYSIS; SHOCK WAVES; SPACECRAFT;

CHEMICAL KINETIC MODEL; CHEMICAL REACTION MODELS; DETAILED MODELING; DETONATION WAVES; NUMERICAL RESULTS; PRESSURE AND TEMPERATURE; REACTION MECHANISM; SINGLE STEP REACTION;

PULSE DETONATION ENGINES;

EID: 84983201931     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (23)

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