Airfoil Boundary-Layer Development and Transition with Large Leading-Edge Roughness
Author:
Affiliation:
1. University of Illinois at Urbana-Champaign, Urbana, Illinois 61801-2935
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.65
Reference19 articles.
1. A study of hairpin vortices in a laminar boundary layer. Part 1. Hairpin vortices generated by a hemisphere protuberance
2. The Effect of Small-Scale Roughness on the Mean Flow Profile of a Laminar Boundary Layer
3. Experiments on transition enhancement by distributed roughness
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