Nonlinear Aeroelastic Response Analysis of Wing with Flared Folding Wingtip-Reference-Cited by-同舟云学术

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Nonlinear Aeroelastic Response Analysis of Wing with Flared Folding Wingtip

Published:2024-05 Issue:3 Volume:37 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Han Junhui¹,Wu Zhigang²,Yang Chao³

Affiliation:

1. Ph.D. Student, School of Aeronautic Science and Engineering, Beijing Univ. of Aeronautics and Astronautics, Beijing 100191, China.

2. Professor, School of Aeronautic Science and Engineering, Beijing Univ. of Aeronautics and Astronautics, Beijing 100191, China (corresponding author).

3. Professor, School of Aeronautic Science and Engineering, Beijing Univ. of Aeronautics and Astronautics, Beijing 100191, China.

Publisher

American Society of Civil Engineers (ASCE)

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-5308

Reference26 articles.

1. Nonlinear Aeroelastic Study for Folding Wing Structures

2. Balatti D. J. D. Ellis S. JiffrI H. Haddad Khodaparast and M. I. Friswell. 2023a. “Active hinged wingtip for gust load alleviation and manoeuvres.” In Proc. AIAA SciTech Forum 2023 2023–2567. Reston VA: American Institute of Aeronautics and Astronautics.

3. Experimental and numerical investigation of an aircraft wing with hinged wingtip for gust load alleviation

4. A Review of Morphing Aircraft

5. Bourdin P. A. Gatto and M. Friswell. 2006. “The application of variable cant angle winglets for morphing aircraft control.” In Proc. 24th AIAA Applied Aerodynamics Conf. Reston VA: American Institute of Aeronautics and Astronautics.

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