Direct solution of two-dimensional Navier-Stokes equations for static aeroelasticity problems
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11331
Reference19 articles.
1. ^owell, E. H. Curtiss, H. C., Scanlaii, R. H., and Sisto, F., A Modern Course in Aeroelasticity, 2nd ed.Kluwer Academic, Boston, MA, 1989, pp.3-50.
2. Integrated aerodynamic-structural design of a transport wing
3. Unsteady aerodynamic and aeroelastic calculations for wings using Euler equations
4. Static aeroelastic analysis of fighter aircraft using a three-dimensional Navier-Stokes algorithm
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