Instability of transonic flow past flattened airfoils-Reference-Cited by-同舟云学术

Instability of transonic flow past flattened airfoils

Published:2013-01-01 Issue:4 Volume:3 Page:
ISSN:2391-5439
Container-title:Open Engineering
language:
Short-container-title:

Author:

Kuzmin Alexander

Abstract

AbstractTransonic flow past a Whitcomb airfoil and two modifications of it at Reynolds numbers of the order of ten millions is studied. The numerical modeling is based on the system of Reynolds-averaged Navier-Stokes equations. The flow simulations show that variations of the lift coefficient versus the angle of attack become more abrupt with decreasing curvature of the airfoil in the midchord region. This is caused by an instability of closely spaced local supersonic regions on the upper surface of the airfoil.

Publisher

Walter de Gruyter GmbH

Subject

Electrical and Electronic Engineering,Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering,Environmental Engineering

Link

http://link.springer.com/content/pdf/10.2478/s13531-013-0124-7.pdf

Reference17 articles.

1. Jameson, A., Airfoils admitting non-unique solutions of the Euler equations, AIAA Paper, 1991, 91–1625, 1–13

2. Hafez, M.M., Guo, W.H., Nonuniqueness of transonic flows, Acta Mechanica, 1999, 138, no. 3–4, 177–184

3. Kuzmin, A., Aerodynamic surfaces admitting jumps of the lift coefficient in transonic flight, in: Hafez M.M., Oshima K., Kwak D. (Eds), Comput Fluid Dynamics Review 2010, World Scientific, Singapure, 2010

4. Kuzmin, A., Non-unique transonic flows over airfoils, Computers and Fluids, 63, 2012, 1–8

5. Jameson, A., Vassberg, J.C., Ou, K., Further studies of airfoils supporting non-unique solutions in transonic flow, AIAA Paper, 2011, 2011–3509, 1–22

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