Development of a Microphone Phased Array Capability for the Langley 14- by 22-foot Subsonic Tunnel
Author:
Affiliation:
1. NASA Langley Research Center
2. Northrop Grumman Corporation
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-2343
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1. Experimental Investigation of the Low-Speed Aerodynamic Characteristics of a 5.8-Percent Scale Hybrid Wing Body Configuration
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4. Effect of directional array size on the measurement of airframe noise components
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