Flow field around spike-tipped bodies

19th AIAA Applied Aerodynamics Conference

Volumn , Issue , 2001, Pages

  Gnemmi, P ^a,c   Srulijes, J ^a,d   Roussel, K ^a,e   Runne, K ^b  

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

^b AIRBUS GROUP INNOVATIONS   (Germany)

^c Aerodynamics and External Ballistics   (France)

^d Shock Tube Department   (France)

^e Aerodynamics and External Ballistics Department   (France)

Author keywords

[No Author keywords available]

Indexed keywords

AIR; ANGLE OF ATTACK; FACINGS; FIGHTER AIRCRAFT; FLOW FIELDS; FLOW PATTERNS; INTERFEROMETRY; MISSILES; NAVIER STOKES EQUATIONS; SHOCK TUBES; SUPERSONIC AIRCRAFT;

AIR-DEFENSE SYSTEM; DIFFERENTIAL INTERFEROMETRY; HIGH ANGLES OF ATTACK; HIGH SURFACE PRESSURE; INFORMATION ACQUISITIONS; NAVIER-STOKES COMPUTATIONS; SHOCK TUBE FACILITY; SURFACE PRESSURE MEASUREMENTS;

DRAG;

EID: 85067319857     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-2464     Document Type: Conference Paper

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