Advanced Laminar Flow Control on a Swept Wing - Useful Crossflow Vortices and Suction
Author:
Affiliation:
1. IAG, Universität Stuttgart
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-3835
Reference13 articles.
1. Mechanisms and passive control of crossflow-vortex-induced transition in a three-dimensional boundary layer
2. The equivalent forcing model for receptivity analysis with application to the construction of a high-performance skin perforation pattern for LFC
3. DNS study of discrete suction in a 3-D boundary layer
4. Smart Suction — an Advanced Concept for Laminar Flow Control of Three-Dimensional Boundary Layers
5. STABILITY AND TRANSITION OF THREE-DIMENSIONAL BOUNDARY LAYERS
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3. Transition control in a three-dimensional boundary layer by direct attenuation of nonlinear crossflow vortices using plasma actuators;International Journal of Heat and Fluid Flow;2016-10
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