Turbulent flow structure characterization of angled injection into a supersonic crossflow

Journal of Spacecraft and Rockets

Volumn 34, Issue 2, 1997, Pages 205-213

  Bowersox, Rodney D W ^a,b,c  

^a AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

^b AICHI INSTITUTE OF TECHNOLOGY   (Japan)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AXIAL FLOW; COMPRESSIBLE FLOW; FLOW MEASUREMENT; FLOW VISUALIZATION; JETS; SCHLIEREN SYSTEMS; SHEAR STRESS; SUPERSONIC AERODYNAMICS; SUPERSONIC FLOW; TURBULENCE; TURBULENT FLOW; VORTEX FLOW;

SCHLIEREN PHOTOGRAPHY; SUPERSONIC CROSSFLOW INJECTION;

FUEL INJECTION;

EID: 0031102143     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3194     Document Type: Article

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