Base Drag Reduction Caused by Riblets on a GAW(2) Airfoil
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/10.2514/2.2403
Reference20 articles.
1. 1Rymer, D., Aircraft Design. A Conceptual Approach, AIAA Educational Series, AIAA, Washington, DC, 1991, pp.255 - 321.
2. Viscous drag reduction using riblets on NACA 0012 airfoil to moderate incidence
3. Turbulent drag reduction using riblets on a supercritical airfoil at transonic speeds
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