Design, Analysis, and Experimental Investigation of a Cyclocopter with Two Rotors

Author:

Lee Choong Hee1,Yong Min Seung2,Lee Jong Won2,Kim Seung Jo3

Affiliation:

1. LIG Nex1, Seongnam-si, Gyeonggi-do 13488, Republic of Korea

2. Korea Aerospace Research Institute, Daejeon 305-333, Republic of Korea

3. Seoul National University, Seoul 151-742, Republic of Korea

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference17 articles.

1. EastmanF. S. “The Full-Feathering Cyclogiro,” University of Washington, Aeronautical Lab. Rept. 317, Seattle, WA, March 1951.

2. EastmanF. S.BurkheimerG.CottarW., Wind Tunnel Tests on a High Pitch Cyclogyro, Univ. of Washington, Aeronautical Lab. Rept. 191-A, Seattle, WA, June 1943.

3. Engineering Experiment Station Series;Kirsten F. K.,1935

4. Modern aviation applications for cycloidal propulsion

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