Unsteady flow structure and vorticity convection over the airfoil oscillating at high reduced frequency

Experimental Thermal and Fluid Science

Volumn 24, Issue 3-4, 2001, Pages 117-129

  Kuo, Cheng Hsiung ^a   Hsieh, J K ^b  

^a NATIONAL CHUNG HSING UNIVERSITY   (Taiwan)

^b Unipac Optoelectronics Corporation   (Taiwan)

Author keywords

Local circulation; Oscillating airfoil; Phase averaged technique; Phase trigger

Indexed keywords

LEADING-EDGE SEPARATION VORTEX;

AIRFOILS; FLOW VISUALIZATION; HEAT CONVECTION; OSCILLATIONS; VORTEX FLOW; WAKES;

UNSTEADY FLOW;

AEROFOIL; CONVECTION; FLOW AROUND OBJECT; FLOW PATTERN; UNSTEADY FLOW; VORTICITY;

EID: 0035330327     PISSN: 08941777     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0894-1777(01)00044-9     Document Type: Article

References (11)

1. Progress in analysis and prediction of dynamic stall
2. Unsteady airfoils
3. A review of recent advances in computational and experimental analysis of dynamic stall. IUTAM, Japan, Tokyo
4. Physics of forced unsteady flow for a NACA 0015 airfoil undergoing constant-rate pitch-up motion
5. Unsteady flow past an airfoil pitching at a constant rate
6. Initial acceleration effects on the flow field development around rapidly pitching airfoil
7. Vortex interactions with walls
8. Development of vortical structure over delta wing with leading-edge flap
9. Vortex formation around an oscillating and translating airfoil at large incidents