An investigation of advanced fuel injection schemes for scramjet combustion

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  Baurle, R A ^a   Fuller, R P ^a   White, J A ^a,c   Chen, T H ^a   Gruber, M R ^b   Nejad, A S ^b,d  

^a Taitech Inc   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c NASA LANGLEY RESEARCH CENTER   (United States)

^d Kaiser Marquardt   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION; FUEL INJECTION; MILITARY AVIATION; MIXING; NAVIER STOKES EQUATIONS; RAMJET ENGINES; STRUTS;

AIR FORCE RESEARCH LAB; FAR FIELD MEASUREMENT; MIXING CHARACTERISTICS; NAVIER-STOKES SOLVER; PRELIMINARY EXPERIMENTAL DATA; SCRAMJET COMBUSTION; TOTAL-PRESSURE LOSS; WRIGHT-PATTERSON AIR FORCE BASE;

COMPUTATIONAL FLUID DYNAMICS;

EID: 85088064620     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-937     Document Type: Conference Paper

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