Thin vs Full Navier-Stokes Computation for High-Angle-of-Attack Aerodynamics
Author:
Affiliation:
1. Technion-Israel Institute of Technology, Haifa 32000, Israel
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.134
Reference15 articles.
1. Pressures Around an Inclined Ogive Cylinder with Laminar, Transitional, or Turbulent Separation
2. Asymmetric Vortices on a Slender Body of Revolution
3. Numerical investigation of the origin of vortex asymmetry
4. Effect of Geometrical Disturbance on Vortex Asymmetry
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