Dynamics of shock dispersion and interactions in supersonic freestreams with counterflowing jets

AIAA Journal

Volumn 47, Issue 6, 2009, Pages 1313-1326

  Daso, Endwell O ^a,e   Pritchett, Victor E ^a   Wang, Ten See ^a   Ota, Dale K ^b   Blankson, Isaiah M ^c,f   Auslender, Aaron H ^d,g  

^a NASA MARSHALL SPACE FLIGHT CENTER   (United States)

^b HYPERCOMP INC   (United States)

^c NASA GLENN RESEARCH CENTER   (United States)

^d NASA LANGLEY RESEARCH CENTER   (United States)

^e Aerospace Flight Systems

^f Mail Stop 5 9 ^*  (United States)

^g Hypersonic Airbreathing Propulsion Branch   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTIVE FLOW CONTROL; AEROTHERMAL; AEROTHERMAL LOADS; BLOW DOWN; BOW SHOCKS; COMPRESSION WAVES; COMPUTATIONAL FLUID DYNAMICS ANALYSIS; COOLING EFFECTS; CRITICAL VALUE; EXIT DIAMETER; HIGH SPEED VEHICLES; JET FLOW RATE; JET INTERACTIONS; JET NOZZLE; PENETRATION MODE; SCHLIEREN IMAGE; STANDOFF DISTANCE; SUPERSONIC AND HYPERSONIC; THERMAL PROTECTION SYSTEM; WAVE DRAGS;

COMPUTATIONAL FLUID DYNAMICS; FLOW CONTROL; FLOW FIELDS; FLOW RATE; FLUID DYNAMICS; GAS DYNAMICS; HEAT FLUX; HEATING; HYPERSONIC AERODYNAMICS; MACH NUMBER; NOZZLES; PLASMA SHOCK WAVES; WIND TUNNELS;

JETS;

EID: 67650901787     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.30084     Document Type: Conference Paper

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