Experimental analysis of the flow of exhaust gas in a hypersonic nozzle

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

Volumn , Issue , 1998, Pages 522-531

  Weisgerber, H ^a   Fischer, M ^a   Magens, E ^a,b   Winandy, A ^a   Forster, W ^a   Beversdorff, M ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

^b RSB Optotechnik GmbH   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AIR; ATMOSPHERIC TEMPERATURE; COHERENT SCATTERING; FLOW VELOCITY; GASES; NOZZLES; RAMAN SCATTERING; RAMAN SPECTROSCOPY; SPACECRAFT;

ATMOSPHERIC CONDITIONS; COHERENT ANTI STOKES RAMAN SCATTERING; EXPERIMENTAL ANALYSIS; FINITE ELEMENT CODES; LASERTWO-FOCUS (L2F); ROTATIONAL TEMPERATURE; SPECIES CONCENTRATION; THERMAL NON-EQUILIBRIUM;

NAVIER STOKES EQUATIONS;

EID: 84983168146     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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