Evaluation of Computational Algorithms Suitable for Fluid-Structure Interactions
Author:
Affiliation:
1. Georgia Institute of Technology, Atlanta, Georgia 30332-0150
2. Massachusetts Institute of Technology, Cambridge, Massachusetts 02139
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2592
Reference23 articles.
1. Fluid-structural interactions using Navier-Stokes flow equations coupled with shell finite element structures
2. Aeroelastic analysis of wings using the Euler equations with a deforming mesh
3. Smith, M. J., Huttsell, L., Schuster, D. M., and Buxton, B. “Development of an Euler/Navier-Stokes Aeroelastic Method for Three-Dimensional Vehicles with Multiple Flexible Surfaces,” AIAA Paper 96-1513,April 1996.
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