Drag reduction using wrinkled surfaces in high Reynolds number laminar boundary layer flows
Author:
Publisher
AIP Publishing
Subject
Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering
Link
http://aip.scitation.org/doi/pdf/10.1063/1.4995566
Reference41 articles.
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4. Blackwell, J. A. “Preliminary study of effects of Reynolds number and boundary-layer transition location on shock-induced separation,” Report No. NASA-TN-D-5003, 1969.
5. Surface Wrinkles for Smart Adhesion
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