Computation of hypersonic propulsion system expansion flows considering hydrogen/air high temperature effects

8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference

Volumn , Issue , 1998, Pages 1-11

  Koschel, Wolfgang W ^a   Link, Thomas ^a   Fox, Ulrich ^a  

^a RWTH AACHEN UNIVERSITY   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATION THEORY; EXPANSION; HIGH TEMPERATURE EFFECTS; SPACECRAFT PROPULSION;

COMPUTATIONAL DOMAINS; FINITE ELEMENT CODES; FINITE-RATE CHEMISTRY; HYPERSONIC PROPULSION SYSTEMS; NON-EQUILIBRIUM EFFECTS; PROPULSION SYSTEM; UNSTRUCTURED GRID; VIBRATIONAL RELAXATION;

HYPERSONIC VEHICLES;

EID: 84983151074     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-1601     Document Type: Conference Paper

References (14)

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