Direct Numerical Simulation of Acoustic Noise Generation from the Nozzle Wall of a Hypersonic Wind Tunnel
Author:
Affiliation:
1. Missouri University of Science and Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-3631
Reference28 articles.
1. Receptivity of a high-speed boundary layer to acoustic disturbances
2. Direct Numerical Simulation on the Receptivity, Instability, and Transition of Hypersonic Boundary Layers
3. Some Statistical Properties of the Pressure Field Radiated by a Turbulent Boundary Layer
4. Effects of High-Speed Tunnel Noise on Laminar-Turbulent Transition
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