Direct numerical simulation of supersonic flow and acoustics over a compression ramp
Author:
Affiliation:
1. Department of Mechanical & Aerospace Engineering, University of Strathclyde, Glasgow G1 1XJ, United Kingdom
2. University of Nicosia, Nicosia CY-2417, Cyprus
3. Air Force Research Laboratory, Wright Patterson AFB, Ohio, 45433-7402, USA
Funder
Air Force Office of Scientific Research
Publisher
AIP Publishing
Subject
Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering
Link
http://aip.scitation.org/doi/am-pdf/10.1063/5.0010548
Reference83 articles.
1. Computational aeroacoustics beneath high speed transitional and turbulent boundary layers
2. Performance of high-order implicit large eddy simulations
3. Implicit large eddy simulation of acoustic loading in supersonic turbulent boundary layers
4. The Structure of Turbulence in a Supersonic Shock-Wave/Boundary-Layer Interaction
5. Unsteadiness of the shock wave structure in attached and separated compression ramp flows
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