Direct Numerical Simulation of a Serrated Nozzle End for Jet-Noise Reduction
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Publication:5745271
DOI10.1007/978-3-540-74739-0_22zbMath1391.76197OpenAlexW172602914WikidataQ59891396 ScholiaQ59891396MaRDI QIDQ5745271
Markus Kloker, Andreas Babucke, Ulrich Rist
Publication date: 5 June 2018
Published in: High Performance Computing in Science and Engineering `07 (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/978-3-540-74739-0_22
Spectral methods applied to problems in fluid mechanics (76M22) Direct numerical and large eddy simulation of turbulence (76F65) Hydro- and aero-acoustics (76Q05)
Cites Work
- DNS of a plane mixing layer for the investigation of sound generation mechanisms
- Noise sources in a low-Reynolds-number turbulent jet at Mach 0.9
- Direct Numerical Simulation of Shear Flow Phenomena on Parallel Vector Computers
- Numerical Investigation of Flow-Induced Noise Generation at the Nozzle End of Jet Engines
- Remarks on disputed numerical results in compressible boundary-layer stability theory
- Sound generation in a mixing layer
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