Euler and Navier-Stokes leeside flows over supersonic delta wings
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia
2. Massachusetts Institute of Technology, Cambridge, Massachusetts
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45784
Reference29 articles.
1. THEORETICAL AND EXPERIMENTAL STUDIES OF CAMBERED AND TWISTED WINGS OPTIMIZED FOR FLIGHT AT SUPERSONIC SPEEDS
2. Navier-Stokes computations of lee-side flows over delta wings
3. Comparison of computations and experimental data for leading edge vortices - Effects of yaw and vortex flaps
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1. Turbulence models for the computation of flow past airplanes;Progress in Aerospace Sciences;1997-01
2. Application of SPLITFLOW unstructured CFD code to Euler predictions of a generic fighter model;13th Applied Aerodynamics Conference;1995-06-19
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