Supercritical airfoil boundary-layer and near-wake measurements
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California
2. McDonnell Douglas Corporation, St. Louis, Missouri
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.44867
Reference11 articles.
1. Experiments on the Flow about a Supercritical Airfoil Including Holographic Interferometry
2. 2Melnik, R.E., Chow, R., and Mead, H.R. "Theory of Viscous Transonic Flow Over Airfoils at High Reynolds Number," AIAA .Paper'77-680,1977.
3. Transonic Flow Past a Symmetrical Airfoil-Inviscid and Turbulent Flow Properties
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