Wave drag of slender star-shaped bodies at moderate supersonic flight velocities-Reference-Cited by-同舟云学术

Wave drag of slender star-shaped bodies at moderate supersonic flight velocities

Published:1984 Issue:5 Volume:18 Page:783-788
ISSN:0015-4628
Container-title:Fluid Dynamics
language:en
Short-container-title:Fluid Dyn

Author:

Foll� M. I.

Publisher

Springer Science and Business Media LLC

Subject

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

Link

http://link.springer.com/content/pdf/10.1007/BF01091003.pdf

Reference12 articles.

1. G. G. Chernyi and A. L. Gonor, ?The determination of body shapes of minimum drag using the Newton and the Busemann pressure laws,? Paper Presented at the Symposium on External Problems in Aerodynamics, Boeing Research Laboratories, Seattle, Washington (1962), p. 23.

2. A. L. Gonor, ?Three-dimensional bodies of least drag at high supersonic velocities,? Prikl. Mat. Mekh.,27, 185 (1963).

3. A. Miele (ed.), Theory of Optimum Aerodynamic Shapes, Academic Press (1965).

4. A. L. Gonor, M. A. Zubin, and N. A. Ostapenko, ?Experimental investigation of aerodynamic characteristics of star-shaped bodies at supersonic velocities,? in: Nonequilibrium Gas Flows and Optimal Body Shapes in Supersonic Flight [in Russian], Izd. MGU, Moscow (1978), pp. 28?39

5. V. I. Lapygin, ?Calculation of supersonic flow over V-shaped wings by the method of stabilization,? Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 3, 180 (1971).

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1. Supersonic aircraft drag reduction;21st Fluid Dynamics, Plasma Dynamics and Lasers Conference;1990-06-18

2. Influence of the shock layer on the viscous drag of star-shaped bodies with planar side panels;Journal of Applied Mechanics and Technical Physics;1986