Variable N-Factor Method for Transition Prediction in Three-Dimensional Boundary Layers
Author:
Affiliation:
1. The Boeing Company, Seattle, Washington 98124-2207
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.973
Reference29 articles.
1. Prediction of transition location for a 2-D Navier-Stokes solver for multi-element airfoil configurations
2. Linear Stability Theory Applied to Boundary Layers
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