An investigation of unsteady vortex flow for a pitching-rolling 70° delta wing

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  Kowal, H J ^a,b   Vakili, A D ^c  

^a ROYAL MILITARY COLLEGE OF CANADA   (Canada)

^b 14 Wing ^*  (Canada)

^c UNIVERSITY OF TENNESSEE SPACE INSTITUTE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; ANGLE OF ATTACK; FLIGHT DYNAMICS; HYSTERESIS; VORTEX FLOW;

OSCILLATORY MOTION; PITCH FREQUENCIES; QUANTITATIVE FLOW VISUALIZATION; REDUCED FREQUENCY; ROYAL MILITARY COLLEGES; UNSTEADY ANALYSIS; UNSTEADY CONDITIONS; UNSTEADY VORTEX FLOWS;

DELTA WING AIRCRAFT;

EID: 84983155065     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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