Effects of Low-Frequency Noise in Crossflow Transition Control
Author:
Affiliation:
1. University of Stuttgart, D-70550 Stuttgart, Germany
Funder
China Scholarship Council
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference37 articles.
1. Basic experiments on transition in three-dimensional boundary layers dominated by crossflow instability
2. Secondary instability of crossflow vortices and swept-wing boundary-layer transition
3. Mechanisms and passive control of crossflow-vortex-induced transition in a three-dimensional boundary layer
4. Transition mechanisms induced by travelling crossflow vortices in a three-dimensional boundary layer
5. STABILITY AND TRANSITION OF THREE-DIMENSIONAL BOUNDARY LAYERS
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