Sidejet Aerodynamic Interaction Effects of the Missile-Reference-Cited by-同舟云学术

Sidejet Aerodynamic Interaction Effects of the Missile

Published:2001-04 Issue:4 Volume:39 Page:611-617
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Kikumoto Kousuke¹,Sentoh Etsuroh¹,Tanaka Hideki²,Takahashi Tatsuo³

Affiliation:

1. Japan Defense Agency, Tokyo 190-8533, Japan

2. IHI Aerospace Company, Ltd., Gunma 370-2398, Japan

3. Kawasaki Heavy Industries, Ltd., Gifu 504-8710, Japan

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.1383

Reference8 articles.

1. Janos, J. “Loads Induced on a Flat-Plate Wing by an Air Jet Exhausting Perpendicularly Through the Wing and Normal to a Free-Stream Flow of Mach Number 2.0,” NASA TN D-649,1961.

2. A study of the interaction of gaseous jets from transverse slots with supersonic external flows.

3. Stagnation temperature and molecular weight effects in jet interaction

4. Experimental investigation of side-jet steering for supersonic and hypersonic missiles

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