Method laminar-turbulent transition control of supersonic boundary layer on a swept wing
Author:
Publisher
Pleiades Publishing Ltd
Subject
Nuclear and High Energy Physics,Radiation
Link
http://link.springer.com/content/pdf/10.1134/S0869864307030031.pdf
Reference11 articles.
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3. M.R. Malik, F. Li, M.M. Choudhari, and C.L. Chang, Secondary instability of crossflow vortices and swept-wing boundary layer transition, J. Fluid Mech., 1999, Vol. 399, P. 85–115.
4. P. Wasserman and M. Kloker, Mechanisms and control of crossflow-vortex induced transition in a three-dimensional boundary layer, J. Fluid Mech., 2002, Vol. 456, P. 49–84.
5. M. Shimagaki, S. Bose, Ya. Kohama, H. Watanabe, and S. Kikuchi, Control of the transition in three-dimensional boundary layer by small-sized roughness alleys, Trans. Jap. Soc. Mech. Engng. B., 2002, Vol. 68, No. 669, P. 1368–1375.
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