Engineering Methods Applied to an Unmanned Combat Air Vehicle Configuration
Author:
Affiliation:
1. Nangia Aero Research Associates, Bristol, England BS8 1QU, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031384
Reference12 articles.
1. X-31 Vector Aircraft, Low Speed Stability & Control, Comparisons of Wind Tunnel Data & Theory (Focus on Linear & Panel Codes)
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