Aerodynamic characteristics of a delta wing in hypersonic flow-Reference-Cited by-同舟云学术

Aerodynamic characteristics of a delta wing in hypersonic flow

Published:1994-03 Issue:2 Volume:35 Page:224-227
ISSN:0021-8944
Container-title:Journal of Applied Mechanics and Technical Physics
language:en
Short-container-title:J Appl Mech Tech Phys

Author:

Kiselev V. Ya.,Maslov A. A.,Shiplyuk A. N.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Link

http://link.springer.com/content/pdf/10.1007/BF02369177.pdf

Reference14 articles.

1. Workshop on Hypersonic Flows for Reentry Problem, Antibes, France (Jan. 22–25, 1990).

2. I. G. Druker, V. D. Zhak, B. A. Sapogov, and Yu. A. Safronov, “Characteristics of the hypersonic nitrogen tunnel at the Institute of Theoretical and Applied Mechanics, Siberian Branch of the Academy of Sciences,” in: Problems in Gas Dynamics [in Russian], No. 5, ITPM SO AN SSSR, Novosibirsk (1975).

3. V. Ya. Kiselev, A. A. Maslov, and A. N. Shiplyuk, “Three-component strain-gauge balance for model testing in a high-temperature gas flow,” Preprint No. 5-92, Institute of Theoretical and Applied Mechanics, Siberian Branch of the Russian Academy of Sciences, Novosibirsk (1992).

4. V. Ya. Kiselev, A. A. Maslov, and A. N. Shiplyuk, “The strain-gage balance for measurement of forces and pitching-moment acting on a model in hypersonic wind tunnel,” in: Proceedings of the International Conference on the Methods of Aerophysical Research [in Russian], Novosibirsk (1992).

5. V. Ya. Kiselev, A. A. Maslov, and A. N. Shiplyuk, “Aerodynamic characteristics of test models at Mach number M=22,” Sib. Fiz.-Tekh. Zh. (Izv. Sib. Otd. Russk. Akad. Nauk), No. 3 (1992).