Effect of amplitude and mean angle-of-attack on the boundary layer of an oscillating aerofoil

Aeronautical Journal

Volumn 112, Issue 1138, 2008, Pages 705-713

  Soltani, M R ^a   Bakhshalipour, A ^a  

^a SHARIF UNIVERSITY OF TECHNOLOGY   (Iran)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BOUNDARY LAYERS; TRANSITION FLOW; TURBOMACHINE BLADES; WIND TUNNELS; WIND TURBINES;

DYNAMIC TRANSITIONS; FREE-STREAM VELOCITY; OSCILLATION FREQUENCY; SPATIAL TEMPORALS; SURFACE PRESSURE DISTRIBUTION; UNSTEADY BOUNDARY LAYER; WIND TUNNEL TESTS; WIND TURBINE BLADES;

ANGLE OF ATTACK;

EID: 59049100887     PISSN: 00019240     EISSN: None     Source Type: Journal    
DOI: 10.1017/S0001924000002670     Document Type: Article

References (14)

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