A High Order Cut-Cell Method for Numerical Simulation of Hypersonic-Boundary Transition with Arbitrary Surface Roughness
Author:
Affiliation:
1. UCLA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-1337
Reference46 articles.
1. Direct Numerical Solution of the Crossflow Instabilities Induced by a Periodic Roughness Array on a swept cylinder: receptivity and stability investigations
2. Discrete Roughness Transition for Hypersonic Flight Vehicles
3. T. Y. Hou, Z. Li, S. Osher, H. Zhao A hybrid method for moving interface problems with application to the Hele-Shawflow. J. ofComp Physics.134:236-252.
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