A Transonic Laminar-Flow Wing Glove Flight Experiment: Overview and Design Optimization
Author:
Affiliation:
1. Texas A&M University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-2667
Reference25 articles.
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2. Compressibility effects on laminar-turbulent boundary layer transition
3. Belisle MJ, Neale TP, Reed HL, Saric WS. 2009 Design of a Swept-Wing Laminar Flow Control Flight Experiment for Transonic Aircraft. AIAA-2010-4381
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