CFD analysis of the HyShot supersonic combustion flight experiment configuration

A Collection of Technical Papers - 14th AIAA/AHI International Space Planes and Hypersonic Systems and Technologies Conference

Volumn 2, Issue , 2006, Pages 1325-1335

  Karl, Sebastian ^a,c,d   Hannemann, Klaus ^a,c,d   Steelant, Johan ^b,d   Mack, Andreas ^b,d  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

^b EUROPEAN SPACE AGENCY   (Netherlands)

^c Spacecraft Section ^*  (Germany)

^d AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

NOZZLE FLOW; TURBULENT MODELING; TURBULENT REACTING FLOW;

COMBUSTION; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; LAMINAR FLOW; NOZZLES; SUPERSONIC AERODYNAMICS;

FLIGHT DYNAMICS;

EID: 33947290017     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (21)

1. Long-Term Advanced Propulsion Concepts and Technologies project investigating high-speed airbreathing propulsion. LAPCAT, coordinated by ESA-ESTEC, is supported by the EU within the 6th Framework Programme Priority 1.4, Aeronautic and Space, Contract no.: AST4-CT-2005-012282.
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