Euler-Based Dynamic Aeroelastic Analysis of Shell Structures
Author:
Affiliation:
1. University of Hertfordshire, Herts, England AL10 9AB, United Kingdom
2. Georgia Institute of Technology, Atlanta, Georgia 30332-0150
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2678
Reference21 articles.
1. AN OVERVIEW OF AEROELASTICITY STUDIES FOR THE NATIONAL AERO-SPACE PLANE
2. Model tests on shell flutter due to flow on both sides
3. Simulation of engine installation flowfields using a three-dimensional Euler/Navier-Stokes algorithm
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2. Numerical Analysis of Store-Induced Limit-Cycle Oscillation;Journal of Aircraft;2004-11
3. Predictions of Store-Induced Limit-Cylce Oscillations Using Euler and Navier-Stokes Fluid Dynamics;44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2003-04-07
4. Evaluation of computational aeroelasticity codes for loads and flutter;39th Aerospace Sciences Meeting and Exhibit;2001-01-08
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