An Improved Neural Network Model for Nonlinear Aeroelastic Analysis-Reference-Cited by-同舟云学术

An Improved Neural Network Model for Nonlinear Aeroelastic Analysis

Published:2003-04-07 Issue: Volume: Page:
ISSN:
Container-title:44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
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Author:

Voitcu Ovidiu,Wong Yau Shu

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-1493

Reference14 articles.

1. Limit Cycle Oscillation Flight Test Results of a Fighter with External Stores

2. Limit Cycle Oscillation Prediction Using Artificial Neural Networks

3. Nonlinear aeroelastic analysis of airfoils: bifurcation and chaos

4. Liu, L. “Mathematical Analysis in Nonlinear Aeroelasticity,” Ph.D. Dissertation,Department of Mathematical and StatisticalSciences, UniversityofAlberta, Edmonton, AB, Canada,December 2001.

5. Neural Network Approach for Nonlinear Aeroelastic Analysis

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