Discrete vortex computation of separated airfoil flow
Author:
Affiliation:
1. Indonesian Aircraft Industries, Bandung, Indonesia
2. Imperial College, London, England
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.9796
Reference10 articles.
1. A discrete vortex method for the non-steady separated flow over an airfoil
2. Discrete-vortex simulation of a turbulent separation bubble
3. Vortex shedding from bluff bodies in oscillatory flow: A report on Euromech 119
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