Theoretical Modeling of Two-Body Interaction in Supersonic Flow-Reference-Cited by-同舟云学术

Theoretical Modeling of Two-Body Interaction in Supersonic Flow

Published:2010-02 Issue:2 Volume:48 Page:258-266
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Fedorov Alexander V.¹,Soudakov Vitaly G.¹,Malmuth Norman D.²

Affiliation:

1. Moscow Institute of Physics and Technology, 140180 Zhukovsky, Russia

2. Teledyne Scientific and Imaging, Thousand Oaks, California 91360

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.40592

Reference21 articles.

1. Nielsen, J. N., Missile Aerodynamics, McGraw-Hill, New York, 1960.

2. Gapcynski, J. P., and Carlson, H. W., A Pressure-Distribution Investigation of the Aerodynamic Characteristics of the Body of Revolution in the Vicinity of a Reflection Plane at Mach Numbers 1.41 and 2.01, NASA Research Memorandum L54129, Jan.1955.

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