Flow past an airfoil with a leading-edge rotation cylinder

Journal of Aircraft

Volumn 39, Issue 6, 2002, Pages 1079-1084

  Du, X ^a   Lee, T ^a   Mokhtarian, F ^b   Kafyeke, F ^b  

^a MCGILL UNIVERSITY   (Canada)

^b BOMBARDIER AEROSPACE   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; ANEMOMETERS; BOUNDARY LAYERS; COMPUTER SIMULATION; DRAG; FLOW MEASUREMENT; FLOW VISUALIZATION; LIFT; PRESSURE MEASUREMENT; ROTATION; WAKES; WIND TUNNELS;

HOT WIRE ANEMOMETRY; LEADING EDGE ROTATION CYLINDER; LIFT TO DRAG RATIO; SMOKE FLOW VISUALIZATION;

AIRFOILS;

EID: 0036873087     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.3040     Document Type: Article

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