Vortex Shedding and Noise Radiation from a Slat Trailing Edge
Author:
Affiliation:
1. Tokyo Metropolitan University, Tokyo 191-0065, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.45777
Reference20 articles.
1. Olson, S., Flint, O., Nelson, T., and Nelson, R. C. "A Preliminary Investigation into Slat Noise Production Mechanisms in a High-Lift Configuration," AIAA Paper 2000-4508.
2. Olson, S., Flint, O., Nelson, T., and Nelson, R. C. "Mechanisms of Slat Noise Production in a 2D Multi-Element Airfoil Configuration," AIAA Paper 2001-2156.
3. Unsteady Flow Computations of a Slat with a Blunt Trailing Edge
4. Time-Accurate Simulations and Acoustic Analysis of Slat Free Shear Layer
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