Unsteady shock-vortex interaction on a flexible delta wing
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/10.2514/3.46247
Reference20 articles.
1. Numerical simulation of vortical flows over a strake-delta wing
2. Numerical simulation of the effects of variation of angle of attack and sweep angle on vortex breakdown over delta wings
3. Computation of vortex-dominated flow for a delta wing undergoing pitching oscillation
4. Vortical flow computations on swept flexible wings using Navier-Stokes equations
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