Turbulence measurements and noise generation in a transonic cryogenic wind tunnel
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia
2. NASA Langley Research Center, Hampton, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.25129
Reference17 articles.
1. Preliminary measurements of velocity, density and total temperature fluctuations in compressible subsonic flow
2. A Summary of Reynolds Number Effects on Some Recent Tests in the Langley 0.3-Meter Transonic Cryogenic Tunnel
3. Cryogenic tunnel measurement of total temperature and pressure
4. Noise Generation in Transonic Tunnels
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1. An algorithm to separate wind tunnel background noise from turbulent boundary layer excitation;Chinese Journal of Aeronautics;2019-09
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