Base flow/underexpanded exhaust plume interaction in a supersonic external flow

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

Volumn , Issue , 1998, Pages 500-510

  Bannink, W J ^a   Houtman, E M ^a   Bakker, P G ^a  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER; ROCKET NOZZLES; ROCKETS; SUPERSONIC AIRCRAFT; TURBULENCE MODELS; WIND TUNNELS;

COMPRESSIBLE TURBULENCE; EXPERIMENTAL RESEARCH; NAVIER-STOKES CODE; NAVIER-STOKES COMPUTATIONS; ROCKET-PROPELLED VEHICLE; STAGNATION PRESSURES; TEST CONDITION; VISUALIZATION RESULTS;

HYPERSONIC VEHICLES;

EID: 84983109662     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-1598     Document Type: Conference Paper

References (9)

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