Multidomain spectral solutions of high-speed flows over blunt cones
Author:
Affiliation:
1. Florida State University, Tallahassee, Florida 32306
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11919
Reference12 articles.
1. A time-dependent computational method for blunt body flows.
2. Spectral methods for the Euler equations - The blunt body problem revisited
3. A spectral multidomain method for the solution of hyperbolic systems
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1. High-order non-uniform grid schemes for numerical simulation of hypersonic boundary-layer stability and transition;Journal of Computational Physics;2003-09
2. Time-accurate simulations of hypersonic boundary layer stability and transition over blunt bodies using implicit parallel algorithms;40th AIAA Aerospace Sciences Meeting & Exhibit;2002-01-14
3. Implicit parallel algorithms for time-accurate simulations of hypersonic boundary layer receptivity over blunt bodies;39th Aerospace Sciences Meeting and Exhibit;2001-01-08
4. Shock-fitted multidomain solution of supersonic flows;Computer Methods in Applied Mechanics and Engineering;1999-07
5. A Stable Penalty Method for the Compressible Navier--Stokes Equations: III. Multidimensional Domain Decomposition Schemes;SIAM Journal on Scientific Computing;1998-01
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