Slat Noise Source Identification
Author:
Affiliation:
1. Aachen University of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-3100
Reference37 articles.
1. Computational Aeroacoustic Analysis of Slat Trailing-Edge Flow
2. Aeroacoustic Wind Tunnel Measurements on a 2D High-Lift Configuration
3. Unsteady Flow Computations of a Slat with a Blunt Trailing Edge
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