Computation of steady and unsteady vortex-dominated flows with shockwaves
Author:
Affiliation:
1. Old Dominion University, Norfolk, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.9929
Reference14 articles.
1. Euler and Navier-Stokes solutions for flow over a conical delta wing
2. Total pressure loss in vortical solutions of the conical Euler equations
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4. Three-dimensional solutions to the Euler equations with one million grid points
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