Effect of Mach number on boundary layer noise
Author:
Affiliation:
1. Paris Institute of Technology
2. National Center for Scientific Research (CNRS)
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-3291
Reference32 articles.
1. Boundary-layer pressures and the Corcos model: a development to incorporate low-wavenumber constraints
2. The character of the turbulent wall pressure spectrum at subconvective wavenumbers and a suggested comprehensive model
3. Direct Computation of Turbulent Boundary Layer Noise
4. The Link Between Wall Pressure Spectra and Radiated Sound from Turbulent Boundary Layers
5. Turbulent boundary-layer noise: direct radiation at Mach number 0.5
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