Shock control bump optimization for a low sweep supercritical wing

Author:

Deng Feng,Qin Ning,Liu XueQiang,Yu XiongQing,Zhao Ning

Publisher

Springer Science and Business Media LLC

Subject

General Engineering,General Materials Science

Reference12 articles.

1. Howe D. Aircraft Conceptual Design Synthesis. London: Professional Engineering Publishing Limited, 2000. 158–159

2. Ashill P R, Fulker J L, Shires A. A novel technique for controlling shock strength of laminar flow aerofoil sections. The First European Symposium on Laminar Flow, Hamburg, March 1992

3. Fulker J L, Ashill P R, Simmons M J. Study of simulated active control of shock waves on an aerofoil. Defence Research Agency Technical Report TR93025. Farnborough: Defence Research Agency, May 1993

4. Fulker J L, Simmons M J. An Experimental Study of Shock Control Methods. DRA/AS/HWA/TR 94007/1, 1994

5. Qin N, Monet D, Shaw S T. 3D Bumps for Transonic Wing Shock Control and Drag Reduction. CEAS Aerospace Aerodynamics Research Conference, Cambridge, UK, 2002

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