Investigation of Lift Offset on Flight Dynamics Characteristics for Coaxial Compound Helicopters
Author:
Affiliation:
1. Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China
2. University of Glasgow, Glasgow, Scotland G12 8QQ, United Kingdom
Funder
National Natural Science Foundation of China
China Scholarships Council
Nanjing University of Aeronautics and Astronautics PhD short-term visiting scholar project
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference31 articles.
1. Compound Helicopter: Insight and Optimization
2. Optimum Design of a Compound Helicopter
3. Design of a Cruise-Efficient Compound Helicopter
4. JohnsonW.MoodieA. M.YeoH. “Design and Performance of Lift-Offset Rotorcraft for Short-Haul Missions,” NASA Ames Research Center Rept. ADA563404, Moffett Field, CA, 2012.
5. Some Approximations to the Flapping Stability of Helicopter Rotors
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