Rotor Design for the Performance Optimization of Canard Rotor/Wing Aircraft

Author:

Lee Jae-Woo,Jeon Kwon-Su,Kim Min-Ji,Byun Yung-Hwan,Kim Chang J.,Yu Yung H.

Publisher

Springer Berlin Heidelberg

Reference10 articles.

1. Smith, C.R.: Hot Cycle Rotor/Wing Composite Research Aircraft. Hughes Tool Company, Aircraft Division, Culver City, CA (1968)

2. Sutton, J.G., Sawicki, A.C.: X-wing Application. In: Presentation submitted to the Sixth Annual Northeast Regional Conference of the Society of Allied Weight Engineers, Smithtown, New York (1985)

3. Schwartz, A.W., Rogers, E.O.: Tipjet VLAR UAV: Technology Development Status. In: Paper presented at the 20th Annual Symposium and Exhibit of the Association for Unmanned Vehicle Systems, Washington, D.C. (1993)

4. Clark, A.M., Barvara, J.V.: The Canard Rotor Wing (CRW) Aircraft – A New Way To Fly. In: AIAA Symposium (2003)

5. Ramon, L.: X-50 Dragonfly Poised For Takeoff. Aerospace America (2002)

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