Design, Analysis, and Experimental Investigation of a Cyclocopter with Two Rotors-Reference-Cited by-同舟云学术

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

Published:2016-09 Issue:5 Volume:53 Page:1527-1537
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

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

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032731

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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