The influence of acceleration and deceleration on shock wave movement on and around aerofoils in transonic flight-Reference-Cited by-同舟云学术

The influence of acceleration and deceleration on shock wave movement on and around aerofoils in transonic flight

Published:2009-06-07 Issue:4 Volume:19 Page:297-305
ISSN:0938-1287
Container-title:Shock Waves
language:en
Short-container-title:Shock Waves

Author:

Roohani Hamed,Skews B. W.

Publisher

Springer Science and Business Media LLC

Subject

General Physics and Astronomy,Mechanical Engineering

Link

http://link.springer.com/content/pdf/10.1007/s00193-009-0207-9.pdf

Reference9 articles.

1. Roohani H., Skews B.W.: Unsteady aerodynamic effects experienced by aerofoils during acceleration and retardation. Proc. I Mech E Part G J. Aerosp. Eng. 222(G5), 631–636 (2008)

2. Lilley G.M., Yates A.H.: Some aspects of noise from supersonic aircraft. J. R. Aeronaut. Soc. (1953)

3. Whitcomb R.T.: A study of the zero-lift drag-rise characteristics of wing-body combinations near the speed of sound. National Advisory Committee for Aeronautics, Report 1273 (1956)

4. Oosthuizen P.H., Carscallen W.E.: Compressible Fluid Flow. McGraw-Hill, New York (1997)

5. Lien F.S., Kalitzin G.: Computation of transonic flow with the v2-f turbulence model. Int. J. Heat Fluid Flow 22, 53–61 (2001)

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