On the stability of the boundary layer on a transonic swept wing
Author:
Affiliation:
1. California Institute of Technology, Jet Propulsion Laboratory, Pasadena, Calif.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1979-264
Reference28 articles.
1. On the stability of three-dimensional boundary layers with application to the flow due to a rotating disk
2. A STABILITY CRITERION FOR THREE-DIMENSIONAL LAMINAR BOUNDARY LAYERS
3. Mass flow requirements for LFC wing design
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