Computational Aeroelasticity Using Modal-Based Structural Nonlinear Analysis-Reference-Cited by-同舟云学术

Computational Aeroelasticity Using Modal-Based Structural Nonlinear Analysis

Published:2020-01 Issue:1 Volume:58 Page:362-371
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Medeiros Renato R.¹,Cesnik Carlos E. S.¹,Coetzee Etienne B.²

Affiliation:

1. University of Michigan, Ann Arbor, Michigan 48109

2. Airbus Operations, Bristol, England BS99 7AR, United Kingdom

Funder

Airbus Americas Inc.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference25 articles.

1. Reexamined Structural Design Procedures for Very Flexible Aircraft

2. NollT. E.BrownJ. M.Perez-DavisM. E.IshmaelS. D.TiffanyG. C.GaierM. “Investigation of the Helios Prototype Aircraft Mishap [online database],” http://www.nasa.gov/pdf/64317main_helios.pdf [retrieved 10 Feb. 2007]; also NASA Press Release http://www.nasa.gov/home/hqnews/2004/sep/HQ_04283_helios_mishap.html.

3. A review on non-linear aeroelasticity of high aspect-ratio wings

4. Nonlinear Flight Dynamics of Very Flexible Aircraft

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