Three-dimensional boundary layer and vortex wake over a cone at high angle of attack: study of asymmetries-Reference-Cited by-同舟云学术

Three-dimensional boundary layer and vortex wake over a cone at high angle of attack: study of asymmetries

Published:1993-02 Issue:4 Volume:14 Page:224-232
ISSN:0723-4864
Container-title:Experiments in Fluids
language:en
Short-container-title:Experiments in Fluids

Author:

Menet J. L.,Menart B.,Tournier C.

Publisher

Springer Science and Business Media LLC

Subject

Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanics of Materials,Computational Mechanics

Link

http://link.springer.com/content/pdf/10.1007/BF00194012.pdf

Reference25 articles.

1. Adrian, R. J.; Fingerson, L. M. 1987: Laser anemometry theory, application and techniques. Publication TSI Incorporated

2. Chapman, G. T.; Keener, E. R.; Malcolm, G. N. 1975: Asymmetric forces on aircraft forebodies at high angles of attack. Some design guides. A.G.A.R.D. CP 199

3. Coe, P. L.; Chambers, J. R.; Letko, W. 1972: Asymmetric lateral directional characteristics of pointed bodies of revolution at high angles of attack. N.A.S.A. T.N. TND-7095, 1–41

4. Cornish, J. J.; Jenkins, M. W. 1978: The application of spanwise blowing for high angles of attack spin recovery. A.G.A.R.D. CP 247

5. Durrani, T. S.; Greated, C. A 1977: Laser systems in flow measurement. Plenum Press

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