Numerical Study of Shock Buffet on Three-Dimensional Wings
Author:
Affiliation:
1. Technion–Israel Institute of Technology, 32000 Haifa, Israel
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053201
Reference38 articles.
1. Transonic Flow about a Thick Circular-Arc Airfoil
2. McDevittJ. B.OkunoA. F. “Static and Dynamic Pressure Measurements on a NACA0012 Airfoil in the Ames High Reynolds Number Facility,” NASA TR-TP-2485, 1985.
3. Experimental Study of Shock Oscillation over a Transonic Supercritical Profile
4. Turbulence model and numerical scheme assessment for buffet computations
5. URANS Computations of Shock-Induced Oscillations Over 2D Rigid Airfoils: Influence of Test Section Geometry
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