Low Reynolds number airfoil performance subjected to wake interference from an upstream airfoil
Author:
Affiliation:
1. Notre Dame, University, IN
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1987-2351
Reference5 articles.
1. on the Effect of Slipstreamon Boundary-Layer Flow," R&M No. 1957,Brit.A.R.C., 1939.
2. Propellers and Vibration on the Extent of Laminar Flow on the NACA 27-212 Airfoil," NACA ACR (WRL-784), 1939.
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