Computational-Fluid-Dynamics-Based Aeroservoelastic Analysis for Gust Load Alleviation-Reference-Cited by-同舟云学术

Computational-Fluid-Dynamics-Based Aeroservoelastic Analysis for Gust Load Alleviation

Published:2018-07 Issue:4 Volume:55 Page:1619-1628
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Chen Gang¹,Zhou Qiang²,Ronch Andrea Da³,Li Yueming¹

Affiliation:

1. Xi’an Jiaotong University, 710049 Xi’an, People’s Republic of China

2. No. 38 Research Institute of China Electronics Technology Group Corporation, 230088 Hefei, People’s Republic of China

3. University of Southampton, Southampton, England, SO17 1BJ, United Kingdom

Funder

Basic Research foundations for the Central Universities

Natural Science Foundation of Shaanxi Provence

Newton Research Collaboration Programme

National Natural Science Foundation of China

National Program on Key Research Project of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C034621

Reference31 articles.

1. ReganC. D.JutteC. V. “Survey of Applications of Active Control Technology for Gust Alleviation and New Challenges for Lighter-Weight Aircraft,” NASA TM-2012-216008, 2012.

2. TheodorsenT. “General Theory of Aerodynamic Instability and the Mechanism of Flutter,” NACA Report, 1935. doi:10.1017/CBO9781107415324.004

3. WrightJ. R.CooperJ. E., Introduction to Aircraft Aeroelasticity and Loads, Vol. 20, Wiley, Chichester, England, U.K., 2008, pp. 457–464. doi:10.1002/9781118700440

4. The Aerodynamic Force on an Airfoil in a Moving Gust

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