Modeling Transition Physics for Laminar Flow Control
Author:
Affiliation:
1. The Boeing Company
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-3832
Reference31 articles.
1. AIRCRAFT LAMINAR FLOW CONTROL
2. 5Van Ingen, J.L. "A suggested semi-empirical method for the calculation of the boundary layer transition region," Report UTH1-74, Univ. of Tech., Delft,1956.
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