Body slot effects on wing-body and wing-tail interference of a typical cannon launched guided projectile
Author:
Affiliation:
1. U.S. Army, Missile Command, Redstone Arsenal, Ala.
2. Martin Marietta Aerospace, Orlando, Fla.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1980-260
Reference8 articles.
1. NA-78-458, May 1978. 4. Buffinqton, R. J. "Transonic Wind
2. Tunnel Test of a Full-Scale Model of t h e COPPERHEAD Projectile," Calspan Corporation Report, AA-4028-W-3, August 1978.
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1. Numerical Investigation of Static and Dynamic Aerodynamic Characteristics for a Guided Projectile with Fin Slot;Advanced Materials Research;2014-07
2. Assessment of two fast aerodynamic codes for guided projectiles;Journal of Spacecraft and Rockets;1987-07
3. Fin gaps and body slots - Effects and modeling for guided projectiles;25th AIAA Aerospace Sciences Meeting;1987-03-24
4. Aerodynamic Properties of an Advanced Indirect Fire System (AIFS) Projectile;Journal of Spacecraft and Rockets;1982-01
5. Aerodynamic properties of an advanced indirect fire system /AIFS/ projectile;19th Aerospace Sciences Meeting;1981-01-12
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