Demonstration by PIV of the Non-Reproducibility of the Flow Field Around an Airfoil Pitching under Deep Dynamic Stall Conditions and Consequences Thereof

Aerospace Science and Technology

Volumn 1, Issue 2, 1997, Pages 125-135

  Wernert, P ^a   Koerber, G ^a   Wietrich, F ^a   Raffel, M ^b   Kompenhans, J ^b  

^a FRENCH GERMAN RESEARCH INSTITUTE OF SAINT LOUIS   (France)

^b GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

Aerodynamics; Conditional sampling phase averaging; Dynamic stall; Dynamic stall vortex; Helicopter; Incompressible flow; Laser Doppler Anemometry (LDA); NACA 0012 profile; Non reproducibility; OA 312 profile; Oscillating airfoil; Pitching motion; Unsteady flow

Indexed keywords

EID: 0031479705     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1270-9638(97)90042-0     Document Type: Article

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