Aeroelastic Wind-Tunnel Test for Aerodynamic Uncertainty Model Validation-Reference-Cited by-同舟云学术

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Aeroelastic Wind-Tunnel Test for Aerodynamic Uncertainty Model Validation

Published:2013-01 Issue:1 Volume:50 Page:47-55
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Wu Zhigang¹,Dai Yuting¹,Yang Chao¹,Chen Lei²

Affiliation:

1. School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, 100191 Beijing, People’s Republic of China

2. Commercial Aircraft Corporation of China, Ltd, Shanghai Aircraft Design and Research Institute, 201210 Shanghai, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C031618

Reference14 articles.

1. Analysis of feedback systems with structured uncertainties

2. Uncertainty Quantification in Aeroelasticity: Recent Results and Research Challenges

3. Analyzing aeroservoelastic stability margins using the mu method

4. A New Approach for Aeroelastic Robust Stability Analysis

5. Match-Point Solutions for Robust Flutter Analysis

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1. Aircraft Active Flutter Suppression: State of the Art and Technology Maturation Needs;Journal of Aircraft;2018-01

2. Alternative Aerodynamic Uncertainty Modeling Approaches for Flutter Reliability Analysis;AIAA Journal;2017-08

3. Strategy for robust gust response alleviation of an aircraft model;Control Engineering Practice;2017-03

4. Uncertainty Analysis of Flutter Predictions With Focus on the AGARD 445.6 Wing;58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2017-01-05

5. Bifurcation Analysis with Aerodynamic-Structure Uncertainties by the Nonintrusive PCE Method;International Journal of Aerospace Engineering;2017

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