Correction Technique of Inertial Force and Moment in Direct Force Measuring Test of Dynamic Aerodynamic Performance of Airfoils-Reference-Cited by-同舟云学术

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Correction Technique of Inertial Force and Moment in Direct Force Measuring Test of Dynamic Aerodynamic Performance of Airfoils

Published:2022-08-22 Issue:4 Volume:23 Page:692-701
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:Int. J. Aeronaut. Space Sci.

Author:

Jiao Yuqin^ORCID,Xiao Chunsheng,Wu Dengke

Funder

National High-tech Research and Development Program

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/s42405-022-00496-x.pdf

Reference20 articles.

1. Carr LW (1988) Progress in the analysis prediction of dynamic stall. J Aircr 25(1):6–17

2. Leishman JG (2000) Principles of helicopter aerodynamics. Cambridge University Press, Cambridge

3. Conlisk AT (2001) Modern helicopter rotor aerodynamics. Prog Aerosp Sci 37(5):419–476

4. Ham ND (1968) Aerodynamic loading in a two-dimensional airfoil during dynamic stall. AIAA J 6(10):1927–1934

5. McCroskey WJ, Pucci SL (1982) Viscous-inviscid interaction on oscillating airfoil in subsonic flow. AIAA J 20(2):167–174

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