Distinctive Features of Flow in the Hypersonic Boundary Layer in the Vicinity of the Plane of Symmetry of a Planar Wing Having a Bend of the Leading Edge

Author:

Dudin G. N.,Ledovskii A. V.

Publisher

Pleiades Publishing Ltd

Subject

Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanical Engineering

Reference8 articles.

1. 1. L. Lees, “On the boundary-Layer Equations in Hypersonic Flow and Their Approximate Solutions,” J. Aeron. Sci. 20(2), 143–145 (1953).

2. 2. K. Stewartson, “On the Motion of a Flat Plate at High Speed in a Viscous Compressible Fluid. I. Impulsive Motion,” Math. Proc. Cambridge Phil. Soc. 51(1), 202–219 (1955).

3. 3. M. D. Ladyzhenskii, “On the Three-Dimensional Hypersonic Flow around Thin Wings,” Prikl. Mat. Mekh. 28(5), 835–844 (1964).

4. 4. V. Ya. Neiland, “On the Theory of the Interaction between a Hypersonic Flow and a Boundary Layer in the Case of Two- and Three-Dimensional Separation Flows. 2. Two- Dimensional Flows and Delta Wings,” Uch. Zap. TsAGI 5(3), 28–39 (1974).

5. 5. S. N. Brown and K. Stewartson, “A Non-Uniqueness of the Hypersonic Boundary Layer,” Quart. J. Mech. Appl. Math. 28(1), 75–90 (1975).

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