Computation of separated duct flows using the boundary-layer equations
Author:
Affiliation:
1. Central Institute of Aviation Motors, Moscow, Russia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12119
Reference14 articles.
1. The integration of the two-dimensional laminar boundary-layer equations past the point of vanishing skin friction
2. Solutions for laminar boundary layers with separation and reattachment
3. New, quasi-simultaneous method to calculate interacting boundary layers
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