Ground testing of the HyShot II scramjet configuration in HEG

15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference

Volumn , Issue , 2008, Pages

  Martinez Schramm, Jan ^a   Karl, Sebastian ^a   Hannemann, Klaus ^a   Steelant, Johan ^b  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

^b EUROPEAN SPACE AGENCY   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION; HEAT TRANSFER; RAMJET ENGINES; SHOCK TESTING; SUPERSONIC AIRCRAFT;

FLIGHT CONFIGURATIONS; FREESTREAM CONDITIONS; GERMAN AEROSPACE CENTERS; HIGH ENTHALPY SHOCK TUNNEL; OPERATING CONDITION; SUPERSONIC COMBUSTION; SURFACE HEAT TRANSFER; SURFACE PRESSURES;

COMPUTATIONAL FLUID DYNAMICS;

EID: 77958513982     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-2547     Document Type: Conference Paper

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