Dynamic flow response due to motion of partial-span Gurney-type flaps

AIAA Journal

Volumn 42, Issue 9, 2004, Pages 1729-1736

  Solovitz, Stephen A ^a,b,c   Eaton, John K ^a,b  

^a STANFORD UNIVERSITY   (United States)

^b Department of Mechanical Engineering ^*  (United States)

^c GE GLOBAL RESEARCH   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AERODYNAMIC LOADS; AIRFOILS; APPROXIMATION THEORY; BOUNDARY LAYERS; CHARGE COUPLED DEVICES; LASER DOPPLER VELOCIMETERS; REYNOLDS NUMBER; TRANSIENTS; VISCOSITY; WAKES;

DYNAMIC FLOW RESPONSE; PARTIAL-SPAN GURNEY-TYPE FLAPS; PARTICLE IMAGE VELOCIMETRY; TRAILING EDGE;

UNMANNED VEHICLES;

EID: 4944251331     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.1200     Document Type: Article

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