Studies on Airframe Noise Generation at High-lift Devices in Relation to Aerodynamic Performances
Author:
Affiliation:
1. Japan Aerospace Exploration Agency
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-2960
Reference41 articles.
1. Airframe noise studies on wings with deployed high-lift devices
2. Takeda, K, Ashcroft, B., G., Zhang, X., Nelson, A., P. "Unsteady Aerodynamics of Slat Cove Flow in a Hihg-lift Device Configuration,"AIAA Paper2001-0706, 2001.
3. Aeroacoustic Measurements of a Wing/Slat Model
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