Aeroacoustic Measurements of a Scaled Half Model at High Reynolds Numbers
Author:
Affiliation:
1. German Aerospace Center (DLR)
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-3748
Reference10 articles.
1. Measurement of Reynolds number effect on airframe noise in the 12-foot pressure wind tunnel
2. High Reynolds Number Aeroacoustics Testing in NASA's National Transonic Facility (NTF)
3. High-Reynolds-Number Cryogenic Wind Tunnel
4. Microphone-array processing for wind-tunnel measurements with strong background noise
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3. Scaling of the Aeroacoustics of High-Speed Trains;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2013
4. Aeroacoustics research in Europe: The CEAS-ASC report on 2011 highlights;Journal of Sound and Vibration;2012-10
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