Aerodynamic characteristics of a canard-controlled missile with a free-spinning tail-Reference-Cited by-同舟云学术

Aerodynamic characteristics of a canard-controlled missile with a free-spinning tail

Published:1998-01-12 Issue: Volume: Page:
ISSN:
Container-title:36th AIAA Aerospace Sciences Meeting and Exhibit
language:
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Author:

Auman Lamar¹,Kreeger Richard¹

Affiliation:

1. U.S. Army, Aviation and Missile Command, Redstone Arsenal, AL

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-410

Reference23 articles.

1. "Free Flight Rocket Technology Program Aeroballistics Directorate FY-74 Activity Report", US Army Missile Command Technical Report TR-RD75-3,July 1974.

2. Burt, J. R., Jr. 'The Effectiveness of Canards for Roll Control", U.S. Army Missile Command Technical Report RD-77-8, November 1976.

3. Burt, J. R., Jr. "An Experimental Investigation of the Aerodynamic Characteristics of Several Nose-Mounted Canard Configurations at Transonic Mach Numbers", U.S. Army Missile Command Technical Report RD-75-2, August 1974.

4. Burt, J. R., Jr. "An Experimental Investigation of the Aerodynamic Characteristics of Several Nose-Mounted Canard Configurations at Supersonic Mach Numbers", U.S. Army Missile Command Technical Report RD-75-17, January 1975.

5. Burt, J. R., Jr. "An Experimental Investigation of the Aerodynamic Characteristics of Several Nose-Mounted Canard Configurations at Supersonic Mach Numbers (1.5through 4.5)", U.S. Army Missile Command Technical Report RD-77-

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