Instability of a three-dimensional boundary layer on a swept wing

Author:

Levchenko V. Ya.,Scherbakov V. A.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Reference17 articles.

1. W. E. Gray, “The nature of the boundary-layer flow at the nose of a swept wing,” in: RAE TM Aero255, Farnborough (1952).

2. N. Gregory, J. T. Stuart, and W. S. Walker, “On the stability of three-dimensional boundary layers with application to flow due to a rotating disk,”Philos. Trans. R. Soc. London,A248, 155–199 (1955).

3. V. V. Kozlov (ed.),Laminar-Turbulent Transition, Springer-Verlag, Berlin (1985).

4. D. Arnal and R. Michel (eds.),Laminar-Turbulent Transition, Springer-Verlag, Berlin (1990).

5. R. Kobayashi (ed.),Laminar-Turbulent Transition, Springer-Verlag, Berlin (1995).

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