Viscous drag reduction using riblets on NACA 0012 airfoil to moderate incidence
Author:
Affiliation:
1. National Aerospace Laboratories, Bangalore 560 017, India.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.13127
Reference23 articles.
1. Near-wall structure of a turbulent boundary layer with riblets
2. Recent Developments in Turbulence Management
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