To Tail or Two Tails? - The Effective Design and Modeling of Yaw Control Devices
Author:
Affiliation:
1. Lockheed Martin
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-4609
Reference11 articles.
Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
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3. Low-Speed Stability and Control of a Reduced Scale Long-Range Supersonic Configuration with Reduced-Size or No Vertical Tail;AIAA Atmospheric Flight Mechanics Conference;2016-01-01
4. A Differential Configuration of Split Drag-Rudders with Variable Bias for Directional Control of Flying-Wing;Applied Mechanics and Materials;2014-09
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