Use of MHD systems in hypersonic aircraft-Reference-Cited by-同舟云学术

Use of MHD systems in hypersonic aircraft

Published:1998-11 Issue:11 Volume:43 Page:1309-1313
ISSN:1063-7842
Container-title:Technical Physics
language:en
Short-container-title:Tech. Phys.

Author:

Fraishtadt V. L.,Kuranov A. L.,Sheikin E. G.

Publisher

Pleiades Publishing Ltd

Subject

Physics and Astronomy (miscellaneous)

Link

http://link.springer.com/content/pdf/10.1134/1.1259189.pdf

Reference8 articles.

1. V. A. Bityurin, J. T. Linebery et al., “Assessment of hypersonic MHD concepts,” AIAA paper 97-2393.

2. R. I. Kurziner, Jet Engines for High Supersonic Flight Speeds [in Russian], Mashinostroenie, Moscow (1989), 264 pp.

3. E. P. Gurijanov and P. T. Harsha, AJAX: New Directions in Hypersonic Technology, AIAA paper 96-4609.

4. E. H. Andrews, C. A. Trexler, and S. Emami, Tests of a Fixed-Geometry Inlet-Combustor Configuration for a Hydrocarbon Fueled Dual-Mode Scramjet, AIAA 94-2817.

5. E. G. Sheikin, Zh. Tekh. Fiz. 62(12), 1 (1992) [Sov. Phys. Tech. Phys. 37, 1133 (1992)].

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