HOT CYCLE ROTOR/WING COMPOSITE RESEARCH AIRCRAFT
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Defense Technical Information Center
Cited by 4 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
1. The Stopped Rotor Concept – A New Look At An Old Idea;AIAA AVIATION 2023 Forum;2023-06-08
2. Rotor Design for the Performance Optimization of Canard Rotor/Wing Aircraft;Computational Science and Its Applications - ICCSA 2006;2006
3. The Canard Rotor Wing (CRW) Aircraft - A New Way to Fly;AIAA International Air and Space Symposium and Exposition: The Next 100 Years;2003-03-11
4. Application of a response surface method to the design of tip jet driven stopped rotor/wing concepts;Aircraft Engineering, Technology, and Operations Congress;1995-08-22
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