Flowfield around spike-tipped bodies for high attack angles at Mach 4.5

Journal of Spacecraft and Rockets

Volumn 40, Issue 5, 2003, Pages 622-631

  Gnemmi, P ^a   Srulijes, J ^a   Roussel, K ^a   Runne, K ^b  

^a FRENCH GERMAN RESEARCH INSTITUTE OF SAINT LOUIS   (France)

^b Flight Mech   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AEROSPACE ENGINEERING; CALCULATIONS; COMPUTER SIMULATION; DRAG; IMAGE SENSORS; INTERFEROMETRY; MANEUVERABILITY; PRESSURE; PRESSURE MEASUREMENT; SHOCK TUBES; TEMPERATURE;

ANGLES OF ATTACK; BLUNT BODY MISSILE; HIGH PRESSURE SHOCK TUNNEL; OPTOELECTRONIC SENSOR; SPIKE TIPPED BODIES;

MISSILES;

EID: 0142180025     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.6910     Document Type: Article

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