Effects of Step Excrescences on Swept-Wing Transition
Author:
Affiliation:
1. Texas A&M University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-2412
Reference19 articles.
1. VKI Lecture Series.;Arnal D
2. 4Carpenter AL. 2009. In-flight receptivity experiments on a 30-degree swept-wing using micron-sized discrete roughness elements. PhDdissertation. TexasA&MUniversity.
3. 5Crawford BK, Duncan Jr. GT, West DE, Saric WS. 2013. Laminar-Turbulent Boundary Layer Transition Imaging Using IR Thermography. Opticsand PhotonicsJournal.
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