Evaluation of wave drag reduction by flow control-Reference-Cited by-同舟云学术

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Evaluation of wave drag reduction by flow control

Published:2006-01 Issue:1 Volume:10 Page:1-8
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Ogawa H.,Babinsky H.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference19 articles.

1. Interaction of shock waves;Bleakney;Rev. Modern Phys.,1949

2. Assessment of shock and boundary layer control concepts for hybrid laminar flow wing design;Dargel,2002

3. J. Délery, R. Bur, The physics of shock wave/boundary layer interaction control: last lessons learned, in: ECCOMASS 2000, Barcelona, 2000

4. Separated shock-boundary-layer interaction control using streamwise slots;Holden;J. Aircraft,2005

5. H.A. Holden, H. Babinsky, Shock/boundary layer interaction control using 3D devices, AIAA Paper 2003-0447, 2003

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