Numerical Solution of Incompressible Turbulent Flow over Airfoils near Stall
Author:
Affiliation:
1. Air Force Wright Aeronautical Laboratories, Wright-Patterson Air Force Base, Ohio
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference10 articles.
1. Numerical solution of the Navier-Stokes equations
2. Calculation of compressible adiabatic turbulent boundary layers
3. Turbulent Boundary-Layer Calculations in Adverse Pressure Gradient Flows
4. An investigation of transonic turbulent boundary layer separation generated on an axisymmetric flow model
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