Modeling and analysis of a geometrically nonlinear joined wing under thrust force-Reference-Cited by-同舟云学术

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Modeling and analysis of a geometrically nonlinear joined wing under thrust force

Published:2023-02 Issue: Volume:544 Page:117369
ISSN:0022-460X
Container-title:Journal of Sound and Vibration
language:en
Short-container-title:Journal of Sound and Vibration

Author:

Liang Jiahua,Bai Junqiang,Sun Zhiwei,Wang Hui,Zhang Bo,Chang Min

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics

Reference42 articles.

1. Conceptual design and aerodynamic study of joined-wing business jet aircraft;Djojodihardjo;J. Mech. Eng. Autom.,2013

2. Challenges, ideas, and innovations of joined-wing configurations: a concept from the past, an opportunity for the future;Cavallaro;Prog. Aerosp. Sci.,2016

3. The joined wing aircraft: an overview;Wolkovitch;J. Aircr.,1986

4. Aerodynamic parametric optimization and analysis of joined-wing configuration;He,2021

5. The lifting system of a PrandtlPlane, part 3: structures made in composites;Frediani,2012

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Mass and Force Lumping: An Essential Enhancement to the Intrinsic Beam Finite Element Discretization;Aerospace;2023-11-13

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