Turbulence Modeling of Flowfields with Massive Surface Ablation
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.57862
Reference26 articles.
1. Heat transfer from a turbulent boundary layer on a porous hemisphere
2. Effect of mass addition on the boundary layer of a hemisphere at Mach 6
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