New Experimental Data of STBLI at DNS/LES Accessible Reynolds Numbers
Author:
Affiliation:
1. Princeton University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-309
Reference15 articles.
1. Measurements of the mean heat transfer in a shock wave-turbulent boundary layer interaction
2. Direct simulation of the turbulent boundary layer along a compression ramp at M = 3 and Reθ = 1685
3. Martin,M.P., S.Xu,andM. Wu,``PreliminaryWorkon DNS andLES ofSTBLI,'' AIAA-2003-3464, June2003.
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