Numerical studies of the flow features and integral aerodynamic characteristics of canard-controlled missiles-Reference-Cited by-同舟云学术

Numerical studies of the flow features and integral aerodynamic characteristics of canard-controlled missiles

Published:2021 Issue: Volume: Page:
ISSN:0094-243X
Container-title:XLIV ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration
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Author:

Voropaev S. N.,Kalugin V. T.

Publisher

AIP Publishing

Link

http://aip.scitation.org/doi/pdf/10.1063/5.0037339

Reference22 articles.

1. Blair A.B. Jr. Wind Tunnel Investigation at Supersonic Speeds of a Canard Controlled Missile with Fixed and Free-Rolling Tail Fins// NASA Technical Paper 1316, September 1978.

2. Blair A. B. Jr. Remote control canard missile with a free-rolling tail brake torque system// Journal of Spacecraft and Rockets. Vol. 18. 26 p. 550–555. November-December 1981.

3. Experimental study of tail-span effects on a canard-controlled missile

4. A. G. Batov [et al.] An experimental study of the aerodynamic characteristics of a canard-controlled missile with differential canards / Defense technology. 2005. 2 6-7. PP. 86–90.

5. Korotkov O. V., Voropaev S. N. The study of the dynamics of rotation in the roll channel of a small-sized canard- controlled missile according to the results of flight tests // Russian Academy of Missile and Artillery Sciences Bulletin. 2013. V.76. 22. PP. 67–73.

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