Wing flutter boundary prediction using unsteady Euler aerodynamic method
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46732
Reference24 articles.
1. Time-accurate unsteady aerodynamic and aeroelastic calculations for wings using Euler equations
2. Static aeroelastic analysis of fighter aircraft using a three-dimensional Navier-Stokes algorithm
3. Numerical simulation of vortical flows on flexible wings
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