Experimental investigation of vortex-tail interaction on a 76/40 degree double-delta wing

17th Applied Aerodynamics Conference

Volumn , Issue , 1999, Pages 444-461

  Ghee, Terence A ^a   Gonzalez, Hugo A ^a   Findlay, David B ^a  

^a Naval Air System Command   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; ANGLE OF ATTACK; POWER SPECTRAL DENSITY; REYNOLDS NUMBER; SPECTRAL DENSITY; TRANSDUCERS; VORTEX FLOW;

ANGLES OF ATTACK; DOUBLE-DELTA WINGS; DYNAMIC PRESSURES; EXPERIMENTAL INVESTIGATIONS; LOW-FREQUENCY; MEASUREMENT LOCATIONS; STRONG DEPENDENCES; VERTICAL TAIL;

DELTA WING AIRCRAFT;

EID: 84964265755     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

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