Active control of boundary-layer instabilities - Use of sensors and spectral controller
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681-0001
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12930
Reference8 articles.
1. Spatial direct numerical simulation of boundary-layer transition mechanisms: Validation of PSE theory
2. Low-storage Runge-Kutta schemes
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