Shock tube study on hydrocarbon free jets using high-speed shadowgraphy

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

Volumn , Issue , 2008, Pages

  Stotz, Ingo ^a   Lamanna, Grazia ^a   Weigand, Bernhard ^a   Steelant, Johan ^b,c  

^a UNIVERSITY OF STUTTGART   (Germany)

^b EUROPEAN SPACE AGENCY   (Netherlands)

^c Propulsion and Aerothermodynamics Division   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

DISPERSIONS; FUELS; HYDROCARBONS;

ELEVATED PRESSURE; INJECTION SYSTEMS; SHOCK ATTENUATION; SHOCK TUBE FACILITY; SPRAY DISPERSION; TEMPORAL DISPERSION; TEST TEMPERATURES; TRANSIENT START-UP;

SHOCK TUBES;

EID: 77958498577     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-2538     Document Type: Conference Paper

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