An efficient evaluation method for wing fuel mass variations effect on transonic aeroelasticity
An efficient evaluation method for wing fuel mass variations effect on transonic aeroelasticity
This paper aims to develop an efficient evaluation method to more intuitively and effectively investigate the influence of the wing fuel mass variations because of fuel burn on transonic aeroelasticity.
Li, Dongfeng
69566740-bed3-4cd6-897d-a93a4a486219
Wang, Zhengzhong
f22bff94-305f-4846-ad87-97f68c70ae5a
Da Ronch, Andrea
a2f36b97-b881-44e9-8a78-dd76fdf82f1a
Chen, Gang
83a5c46f-13cc-4be3-ad5b-698a69e82b8e
Li, Dongfeng
69566740-bed3-4cd6-897d-a93a4a486219
Wang, Zhengzhong
f22bff94-305f-4846-ad87-97f68c70ae5a
Da Ronch, Andrea
a2f36b97-b881-44e9-8a78-dd76fdf82f1a
Chen, Gang
83a5c46f-13cc-4be3-ad5b-698a69e82b8e
Li, Dongfeng, Wang, Zhengzhong, Da Ronch, Andrea and Chen, Gang
(2022)
An efficient evaluation method for wing fuel mass variations effect on transonic aeroelasticity.
Aircraft Engineering and Aerospace Technology.
(doi:10.1108/AEAT-08-2021-0227).
Abstract
This paper aims to develop an efficient evaluation method to more intuitively and effectively investigate the influence of the wing fuel mass variations because of fuel burn on transonic aeroelasticity.
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e-pub ahead of print date: 1 February 2022
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Local EPrints ID: 454948
URI: http://eprints.soton.ac.uk/id/eprint/454948
ISSN: 0002-2667
PURE UUID: dcbd9fba-34bd-4a28-b953-6c89dda8b236
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Date deposited: 02 Mar 2022 17:44
Last modified: 03 Mar 2022 02:44
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Author:
Dongfeng Li
Author:
Zhengzhong Wang
Author:
Gang Chen
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