Laminar boundary layer in a flow past an aerofoil with a circular cavity

Author:

Bunyakin A. V.

Publisher

Springer Science and Business Media LLC

Subject

Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanical Engineering

Reference9 articles.

1. J. Z. Wu, A. D. Vakili, and J. M. Wu, “Review of the physics of enhancing vortex lift by unsteady excitation,” Progr. Aerosp. Sci.,28, No. 1, 73–131 (1991).

2. S. I. Chernyshenko, “Stabilization of trapped vortices by alternating blowing suction,” Phys. Fluids,7, No. 4, 802–807 (1995).

3. A. V. Bunyakin, S. I. Chernyshenko, and G. Yu. Stepanov, “Inviscid Batchelor-model flow past an aerofoil with a vortex trapped in a cavity,” J. Fluid Mech.,323, 367–376 (1996).

4. S. I. Chernyshenko, “Separated flow over a backward-facing step whose height is much greater than the thickness of the lower sublayer of the interaction zone,”Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 4, 25–30 (1991).

5. S. I. Chernyshenko, “The asymptotic form of the stationary separated circumfluence of a body at high Reynolds number,”Prikl. Materm. Mekh.,52, No. 5, 958–966.

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1. Simultaneous Effect of Suction and Cavity on Controlling Flow Separation Over NACA 0012 Airfoil – a CFD Approach;GAZI UNIVERSITY JOURNAL OF SCIENCE;2020-07-15

2. The radiating pressure field of a turbulent cylindrical cavity flow;14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference);2008-05-05

3. Noise Sources from a Cylindrical Cavity;13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference);2007-05-21

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