High-Reynolds Number Aeroacoustic Testing Under Pressurised Cryogenic Conditions in PETW
Author:
Affiliation:
1. German Aerospace Center (DLR)
2. European Transonic Windtunnel (ETW)
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-107
Reference15 articles.
1. Measurement of Reynolds number effect on airframe noise in the 12-foot pressure wind tunnel
2. Aeroacoustic Measurements of a Scaled Half Model at High Reynolds Numbers
3. High Reynolds Number Aeroacoustics Testing in NASA's National Transonic Facility (NTF)
4. Microphone-Array Measurements in a Cryogenic Wind Tunnel
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1. Microphone Array Measurement in European Transonic Wind Tunnel at Flight Reynolds Numbers;AIAA Journal;2017-01
2. Concept for Measuring Aeroacoustic Noise Transmission in Trains Derived from Experience Gained in Aircraft Testing;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2015
3. Real-Flight Reynolds Number Microphone-Array Measurements on a Scaled Model in ETW;52nd Aerospace Sciences Meeting;2014-01-10
4. Aeroacoustic Measurements of a Scaled Half-Model at High Reynolds Numbers;AIAA Journal;2013-12
5. Aeroacoustics research in Europe: The CEAS-ASC report on 2011 highlights;Journal of Sound and Vibration;2012-10
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