Modifications to the DLR high enthalpy shock tunnel HEG for measurements on supersonic combustion

10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference

Volumn , Issue , 2001, Pages

  Beck, W H ^a   Hannemann, K ^a   Weiland, M ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

ENTHALPY; FLIGHT SIMULATORS; NOZZLE DESIGN; RAMJET ENGINES; SHOCK TESTING; SUPERSONIC AIRCRAFT;

DESIGN STUDIES; FULL SIMULATIONS; GROUND TESTING; HIGH ENTHALPY SHOCK TUNNEL; LOW ENTHALPIES; OPTICAL DIAGNOSTICS; PHYSICAL PHENOMENA; SUPERSONIC COMBUSTION;

COMBUSTION;

EID: 85087190486     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-1860     Document Type: Conference Paper

References (12)

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