Turbulence Model Predictions of Strongly Curved Flow in a U-Duct
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681-2199
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1115
Reference36 articles.
1. Investigation of Confluent Boundary Layers in High-Lift Flows
2. Longitudinal curvature effects in turbulent boundary layers
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