Flow visualization over a thick blunt trailing-edge airfoil with base cavity at low Reynolds numbers using PIV technique

Author:

Taherian Gholamhossein,Nili-Ahmadabadi Mahdi,Karimi Mohammad Hassan,Tavakoli Mohammad Reza

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Condensed Matter Physics

Reference23 articles.

1. Aravind A, Al-Garni A (2009) Experimental investigation of the effect of base cavities on the base pressure and wake of a two-dimensional bluff body. Adv Fluid Mech Heat Mass Transf 10:366–373

2. Baker J, Dam C (2008) Drag reduction of blunt trailing-edge airfoils. Bluff Bodies Aerodyn Appl, Milano, pp 20–24

3. Bourgoyne D, Ceccio S, Dowling D, Jessup S, Park J, Brewer W, Pankajakshan R (2000) Hydrofoil turbulent boundary layer separation at high Reynolds number. In: Proceedings of the 23rd symposium on naval hydrodynamics, Val de Reuil, France

4. Cai J, Chng T, Tsia H (2008) On vortical flows shedding from a bluff body with a wavy trailing edge. Phys Fluids 20:064102

5. Cooperman A, McLennan A, Chow R, Baker J, Dam C (2010) Aerodynamic performance of thick blunt trailing edge airfoils. 28th AIAA Applied Aerodynamics Conference. AIAA 2010-4228

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