Numerical Investigation on Aerodynamic Performance and Interaction of a Lift-Offset Coaxial Rotor in Forward Flight-Reference-Cited by-同舟云学术

Numerical Investigation on Aerodynamic Performance and Interaction of a Lift-Offset Coaxial Rotor in Forward Flight

Published:2022-03-01 Issue:2 Volume:23 Page:255-264
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:Int. J. Aeronaut. Space Sci.

Author:

Qi Haotian^ORCID,Wang Ping,Jiang Linsong

Funder

National Natural Science Foundation of China

Foundation of Key Laboratory of Aerodynamic Noise Control

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/s42405-022-00444-9.pdf

Reference31 articles.

1. Ho JC, Yeo H (2020) Analytical study of an isolated coaxial rotor system with lift offset. Aerosp Sci Technol 100:105818

2. Bagai A (2008) Aerodynamic design of the X2 technology demonstrator main rotor blade. Paper presented at the 64th American Helicopter Society Annual Forum, Montréal, Canada, Apr 29–May 1

3. Burgess RK (2004) The ABC™ Rotor – A historical perspective. Paper presented at the 60th American Helicopter Society Annual Forum, Baltimore, MD, USA, 7–10 June

4. Ho JC, Yeo H (2020) Rotorcraft comprehensive analysis calculations of a coaxial rotor with lift offset. Int J Aeronaut Space 21(2):418–438

5. Schmaus JH, Chopra I (2015) Aeromechanics for a high advance ratio coaxial helicopter. Paper presented at the 71st American Helicopter Society Annual Forum, Virginia Beach, VA, USA, 5–7 May

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