Analytical approximation of two-dimensional separated turbulent boundary-layer velocity profiles
Author:
Affiliation:
1. Sverdrup Technology, Inc., Arnold Air Force Station, Tennessee
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.8177
Reference14 articles.
1. Simultaneous Solution of the Boundary Layer and Freestream with Separated Flow
2. A new boundary-layer inviscid iteration technique for separated flow
3. Prediction of Incompressible Turbulent Separating Flow
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