Vortical flows about a long cylinder at M = 3.5 and alpha = 18 deg
Author:
Affiliation:
1. U.S. Navy, Naval Surface Warfare Center, Silver Spring, MD
2. Royal Aerospace Establishment, Bedford, England
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1991-1808
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1. Implicit Finite-Difference Simulations of Three-Dimensional Compressible Flow
2. Navier-Stokes Solution of a Slender Body of Revolution at Incidence
3. Recent improvements in efficiency, accuracy, and convergence for implicit approximate factorization algorithms
4. Numerical simulation of unsteady, viscous, high-angle-of-attack flows using a partially flux-split algorithm
5. Computation of turbulent supersonic flows around pointed bodies having crossflow separation
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