A Testbed for large scale and high Reynolds number Airframe Noise Research
Author:
Affiliation:
1. German Aerospace Center (DLR)
2. EADS
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-2260
Reference11 articles.
1. Dobrzynski, W., Kiyoshi, N., Gehlhar, B., Buschbaum, A. " Airframe Noise Studies on Wings with Deployed High-Lift Devices".AIAA 98-2337,June2-e4,Toulouse,France,1998.
2. Ahlefeldt Th., Lauterbach, A., Koop L. „Aeroacoustic Measurements of a Scaled Half Model at High Reynolds Numbers",AIAA 2010-3748,16th AIAA/CEASAroacousticsConference,7-9June2010,Stockholm,Sweden
3. Correction of open jet wind tunnel measurements for shear layer refraction
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