Effects of Step Excrescences on a Swept Wing in a Low-Disturbance Wind Tunnel
Author:
Affiliation:
1. Texas A&M University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-0910
Reference20 articles.
1. VKI Lecture Series.;Arnal D
2. Passive control of transition in three-dimensional boundary layers, with emphasis on discrete roughness elements
3. 3Drake A, Westphal RV, Zuniga FA, Kennelly RA, Koga DJ. 1996. Wing Leading Edge Joint Laminar Flow Tests. NASA TM 4762.
4. An Approach to Measuring the Effects of Surface Steps on Transition Using a Propelled-Model
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