Aerodynamics of missiles with offset fin configurations
Author:
Affiliation:
1. USAF, Armament Laboratory, Eglin AFB, FL
2. Arrow Tech Associates, South Burlington, VT
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1989-3367
Reference12 articles.
1. West,K.O.andWhyteR.H. "FreeFlight and Wind TunnelTest of a Missile Configuration at Subsonic and Transonic Mach Nmbers with
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