Numerical Investigations of Bump Effects on the Performance of Double-Ended Airfoils and ABC Rotors-Reference-Cited by-同舟云学术

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Numerical Investigations of Bump Effects on the Performance of Double-Ended Airfoils and ABC Rotors

Published:2023-12-02 Issue: Volume: Page:
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:Int. J. Aeronaut. Space Sci.

Author:

Yuan Xin,Zhao Guoqing,Zhao Qijun^ORCID

Funder

National Natural Science Foundation of China

National Key Laboratory Foundation of China

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering

Link

https://link.springer.com/content/pdf/10.1007/s42405-023-00680-7.pdf

Reference33 articles.

1. Cheney MC (1969) The ABC helicopter. J Am Helicopter Soc 14(4):10–19. https://doi.org/10.4050/JAHS.14.4.10

2. Ruddell AJ, Groth W, McCutcheon R (1981) Advancing blade concept technology demonstrator. In: Proceedings of U.S. Army Aviation Research and Development Command, Fort Eustis, Virginia

3. Ruddell AJ (1977) Advancing blade concept (ABC™) development. J Am Helicopter Soc 22:13–23. https://doi.org/10.4050/JAHS.22.1.13

4. Felker III FF (1981) Performance and Loads Data from a Wind Tunnel Test of a Full-Scale, Coaxial, Hingeless Rotor Helicopter. NASA Report, NASA TM-81329 (also USAARADCOM TR 81-A-27)

5. Ruddell AJ (1981) XH-59A ABC Technology Demonstrator Altitude Expansion and operational tests. US Army Report, USAAVRADCOM TR 81-D-35

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