Joined-Wing Aeroelastic Design with Geometric Nonlinearity-Reference-Cited by-同舟云学术

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Joined-Wing Aeroelastic Design with Geometric Nonlinearity

Published:2005-07 Issue:4 Volume:42 Page:832-848
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Blair Maxwell¹,Canfield Robert A.²,Roberts Ronald W.³

Affiliation:

1. U .S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433-7542

2. Air Force Institute of Technology, Wright–Patterson Air Force Base, Ohio 45433-7765

3. U .S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45431-7542

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.2199

Reference22 articles.

1. The joined wing - An overview

2. Preliminary weight estimation of conventional and joined wings usingequivalent beam models

3. Aeroelasticity of joined-wing airplane configurations - Past work and future challenges - a survey

4. Structural optimization for joined-wing synthesis

5. A Joined-Wing Structural Weight Modeling Study

Cited by 73 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. Aero-structural design of joined-wing aircraft based on high-fidelity model;Chinese Journal of Aeronautics;2023-11

2. Modeling and analysis of a geometrically nonlinear joined wing under thrust force;Journal of Sound and Vibration;2023-02

3. A Gaussian process regression reduced order model for geometrically nonlinear structures;Mechanical Systems and Signal Processing;2023-02

4. Flutter Analysis of a 3D Box-Wing Aircraft Configuration;International Journal of Structural Stability and Dynamics;2021-12-29

5. Aeroelastic Optimization Design of the Global Stiffness for a Joined Wing Aircraft;Applied Sciences;2021-12-12

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