Active flow control using high-frequency compliant structures

Journal of Aircraft

Volumn 41, Issue 3, 2004, Pages 603-609

  Osborn, Russell F ^a,d   Kota, Sridhar ^a,d   Hetrick, Joel A ^a,d   Geister, Donald E ^b,e   Tilmann, Carl P ^c,f   Joo, Jinyong ^c,g  

^a FlexSys Inc   (United States)

^b UNIVERSITY OF MICHIGAN   (United States)

^c AIR FORCE RESEARCH LABORATORY   (United States)

^d North Campus ^*  (United States)

^e Aerospace Engineering Department   (United States)

^f Building 45   (United States)

^g Air Vehicles Directorate   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AERODYNAMICS; BOUNDARY LAYERS; INTELLIGENT MATERIALS; PERTURBATION TECHNIQUES; PIEZOELECTRIC DEVICES; PRESSURE DISTRIBUTION; TURBULENT FLOW; VORTEX FLOW; WINGS;

BOUNDARY-LAYER SEPARATION; PRESSURE COEFFICIENTS; PRESSURE TAPS; VOICE-COIL ACTUATORS;

FLOW CONTROL;

EID: 3042756717     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.111     Document Type: Article

References (17)

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