Contouring spike nozzles and determining the optimal direction of their primary flows-Reference-Cited by-同舟云学术

Contouring spike nozzles and determining the optimal direction of their primary flows

Published:2007-04 Issue:2 Volume:42 Page:321-329
ISSN:0015-4628
Container-title:Fluid Dynamics
language:en
Short-container-title:Fluid Dyn

Author:

Kraiko A. N.,Tillyayeva N. I.

Publisher

Pleiades Publishing Ltd

Subject

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

Link

http://link.springer.com/content/pdf/10.1134/S0015462807020172.pdf

Reference20 articles.

1. G.V.R. Rao, “Spike Nozzle Contour for Optimum Thrust,” Planet. Space Sci. 4, 92–101 (1961).

2. H. Greer, “Rapid Method for Plug Nozzle Design,” ARS J. 31, 560 (1961).

3. G. Angelino, “Approximate Method for Plug Nozzle Design,” AIAA J. 2, 1834 (1964).

4. V.M. Borisov, “System of Bodies with Minimum Wave Drag,” Inzh. Zh., 5, 1028 (1965).

5. A.L. Gonor and A.N. Kraiko, “Some results of the study of optimal shapes at supersonic and hypersonic velocities,” in: A. Miele (ed.) Theory of Optimal Aerodynamic Shapes [in Russian], Mir, Moscow (1969), 455–492.

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