Effects of Nozzle geometry on parallel injection into a supersonic flow

Journal of Propulsion and Power

Volumn 12, Issue 6, 1996, Pages 1159-1168

  Glawe, Diana D ^a,d   Samimy, Mo ^a,d   Nejad, Abdollah S ^b,d,e   Chen, Tzong H ^c,d  

^a OHIO STATE UNIVERSITY   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c Taitech Inc   (United States)

^d Department of Mechanical Engineering ^*

^e Experimental Research Branch

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION; COMBUSTORS; COMPUTER SIMULATION; EFFECTS; NOZZLES; SUPERSONIC FLOW; THREE DIMENSIONAL; VORTEX SHEDDING; WAKES;

ELLIPTIC NOZZLE; MACH NUMBERS;

FUEL INJECTION;

EID: 0030285521     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/3.24156     Document Type: Article

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