Prediction of the turbulent near-wake of a symmetrical aerofoil
Author:
Affiliation:
1. National Physical Laboratory, Teddington, England
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.5931
Reference7 articles.
1. The flow in a turbulent boundary layer after a change in surface roughness
2. Simple Phenomenological Theory of Turbulent Shear Flows
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