Rapid Engineering Approach to Modeling Hypersonic Laminar-To-Turbulent Transitional Flows
Author:
Affiliation:
1. Combustion Research and Flow Technology, Inc., Pipersville, Pennsylvania 18947
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.1854
Reference37 articles.
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3. Predictions of Channel and Boundary-Layer Flows with a Low-Reynolds-Number Turbulence Model
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