Numerical aspects of nonlinear flexible aircraft flight dynamics modeling-Reference-Cited by-同舟云学术

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Numerical aspects of nonlinear flexible aircraft flight dynamics modeling

Published:2013-04-05 Issue: Volume: Page:
ISSN:
Container-title:54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
language:
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Author:

Simpson Robert J.¹,Palacios Rafael¹

Affiliation:

1. Imperial College London

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-1634

Reference44 articles.

1. Nonlinear Flight Dynamics of Very Flexible Aircraft

2. Nonlinear Aeroelastic Response of High-aspect-ratio Flexible Wings

3. Nonlinear-Aerodynamics/Nonlinear-Structure Interaction Methodology for a High-Altitude Long-Endurance Wing

4. Dynamic Response of Highly Flexible Flying Wings

Cited by 14 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. Rapid dynamic aeroelastic response analysis of the highly flexible wing with distributed propellers influence;The Aeronautical Journal;2024-04-24

2. An Investigation on Gust Load Alleviation Systems for Very Flexible Aircraft;AIAA SCITECH 2024 Forum;2024-01-04

3. LQG-based Gust Load Alleviation Systems for Very Flexible Aircraft;AIAA SCITECH 2023 Forum;2023-01-19

4. Modelling and Numerical Enhancements on a UVLM for Nonlinear Aeroelastic Simulation;AIAA SCITECH 2022 Forum;2022-01-03

5. Fast flutter evaluation of very flexible wing using interpolation on an optimal training dataset;AIAA SCITECH 2022 Forum;2022-01-03

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