Alleviation of rotor blade dynamic stall via trailing edge flap flow control

41st Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2003, Pages

  Feszty, Daniel ^a   Gillies, Eric A ^a   Vezza, Marco ^a  

^a UNIVERSITY OF GLASGOW   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; COMPUTATIONAL FLUID DYNAMICS; DAMPING; FLIGHT ENVELOPES; FLOW CONTROL; TURBOMACHINE BLADES;

DISCRETE VORTEX METHOD; FLOW CONTROL TECHNIQUES; HELICOPTER ROTOR BLADES; NEGATIVE DAMPING; PITCHING MOMENTS; REDUCED FREQUENCY; ROTOR BLADE DYNAMICS; TRAILING EDGE FLAPS;

VORTEX FLOW;

EID: 85088754631     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-50     Document Type: Conference Paper

References (16)

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