Wall curvature and transition effects in turbulent boundary layers
Author:
Affiliation:
1. Douglas Aircraft Company, Long Beach, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.6438
Reference13 articles.
1. A Finite-Difference Method for Calculating Compressible Laminar and Turbulent Boundary Layers
2. Calculation of Compressible Turbulent Boundary Layers with Heat and Mass Transfer
3. Computation of incompressible turbulent boundary layers at low Reynolds numbers
4. Extension of Emmons' spot theory to flows on blunt bodies
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