Flight Test Experiments on Discrete Roughness Element Technology for Laminar Flow Control
Author:
Affiliation:
1. Texas A&M University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-0539
Reference34 articles.
1. Passive control of transition in three-dimensional boundary layers, with emphasis on discrete roughness elements
2. Experiments in nonlinear saturation of stationary crossflow vortices in a swept-wing boundary layer
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