Numerical simulation of the influence of the control surfaces deflection on the aerodynamics of a slender axisymmetric configuration-Reference-Cited by-同舟云学术

Numerical simulation of the influence of the control surfaces deflection on the aerodynamics of a slender axisymmetric configuration

Published:2016-01 Issue:1 Volume:23 Page:49-58
ISSN:0869-8643
Container-title:Thermophysics and Aeromechanics
language:en
Short-container-title:Thermophys. Aeromech.

Author:

Mazhul I. I.,Volkov V. F.,Zvegintsev V. I.,Ivanov I. V.

Publisher

Pleiades Publishing Ltd

Subject

Nuclear and High Energy Physics,Radiation

Link

http://link.springer.com/content/pdf/10.1134/S0869864316010066.pdf

Reference7 articles.

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3. A. Naveed, G. Balu, P. Theerthamalai, and R.D. Sampath, Investigation of effect of strakes on aerodynamic characteristics at high angles of attack. in: Proc. 6th Symp. on Applied Aerodynamics and Design of Aerospace Vehicles, 21-23 November, 2013, India, P. 59–64.

4. P. Kumar and J.K. Prasad, Effect of height of trip on side force over a slender body at subsonic speed, in: Proc. 6th Symp. on Applied Aerodynamics and Design of Aerospace Vehicles, 21-23 November 2013, India, P. 30–34.

5. D.K. Ghosh, S. Kandasamy, K.N. Swaroop, and D.T. Jaya, Numerical validation study and analysis of hypersonic missile configuration at Mach 5 to 7. in: Proc. 6th Symp. on Applied Aerodynamics and Design of Aerospace Vehicles, 21-23 November, 2013, India, P. 350–358.

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