Vortex-Generator Models for Zero- and Adverse-Pressure-Gradient Flows
Author:
Affiliation:
1. Royal Institute of Technology, 100 44 Stockholm, Sweden
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J051169
Reference28 articles.
1. Pearcey, H. H., Boundary Layer and Flow Control, Its Principles and Applications. Part 4: Shock-Induced Separation and Its Prevention by Design and Boundary Layer Control, edited by G. V. Lachmann, Pergamon, Oxford, 1961, pp.1170-1344.
2. Experimental study of the development of longitudinal vortex pairs embedded in a turbulent boundary layer
3. Review of research on low-profile vortex generators to control boundary-layer separation
4. Control of a decelerating boundary layer. Part 1: Optimization of passive vortex generators
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