Reibungsfreie Hyperschallstr�mung um Profile mit scharfer Vorderkante

Author:

Schneider W.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Computational Mechanics

Reference19 articles.

1. Epstein, P. S.: On the Air Resistance of Projectiles. Proc. Natl. Acad. Sci.17, 532 (1931).

2. Eggers, A. J., andC. A. Syvertson: Inviscid Flow about Airfoils at High Supersonic Speeds. NACA TN 2646, 1952; NACA TR 1123, 1953.

3. Rand, R. C.: Prandtl-Meyer Flow behind a Curved Shock Wave. J. Math. and Phys.29, Nr. 2, 124 (1950).

4. Munk, M. M., andR. C. Prim: Surface-Pressure Gradient and Shock-Front Curvature at the Edge of a Plane Ogive with Attached Shock Front. J. Aeron. Sci.15, Nr. 11, 691 (1948).

5. Kraus, S.: An Analysis of Supersonic Flow in the Region of the Leading Edge of Curved Airfoils, Including Charts for Determing Surface-Pressure Gradient and Shock-Wave Curvature. NACA TN 2729, 1952; NACA TR 1123, 1953.

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1. Hyperschallströmung;Spezialgebiete der Gasdynamik;1977

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