Shallow and deep dynamic stall for flapping low Reynolds number airfoils

Experiments in Fluids

Volumn 46, Issue 5, 2009, Pages 883-901

  Ol, Michael V ^a   Bernal, Luis ^b   Kang, Chang Kwon ^b   Shyy, Wei ^b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b UNIVERSITY OF MICHIGAN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DIRECT FORCE MEASUREMENTS; DYE INJECTIONS; DYNAMIC STALLS; FLOW REATTACHMENTS; FLOW THEORIES; FLOW-FIELD; FLUID PHYSICS; GENERAL TRENDS; LAMINAR SEPARATIONS; LEADING-EDGE VORTICES; LIFT COEFFICIENTS; LOW REYNOLDS NUMBERS; PARTICLE-IMAGE VELOCIMETRY; REDUCED FREQUENCIES; REYNOLDS NUMBER EFFECTS; REYNOLDS-AVERAGED NAVIER-STOKES; TIME HISTORY; TWO-DIMENSIONAL; VELOCIMETRY; WATER TUNNELS;

AIRFOILS; EXPERIMENTS; FLOW SEPARATION; FLOW VISUALIZATION; FORCE MEASUREMENT; LIFT; REYNOLDS NUMBER; SIZE SEPARATION; TUNNELS; VELOCIMETERS; VELOCITY MEASUREMENT;

VORTEX FLOW;

EID: 67349114849     PISSN: 07234864     EISSN: None     Source Type: Journal    
DOI: 10.1007/s00348-009-0660-3     Document Type: Article

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