A General Framework for the Optimal Control of Unsteady Flows with Applications
Author:
Affiliation:
1. University of Toronto Institute for Aerospace Studies
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-1128
Reference31 articles.
1. Computational Aeroacoustic Analysis of Slat Trailing-Edge Flow
2. Unsteady Flow Computations of a Slat with a Blunt Trailing Edge
3. The harmonic adjoint approach to unsteady turbomachinery design
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