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1 Ergebnisse
1
Aeroacoustic Analysis of a Closely Installed Chevron Nozzle..:
Lindblad, D
;
Sherwin, S
;
Cantwell, C
...
https://arc.aiaa.org/doi/abs/10.2514/6.2023-3831. , 2023
Link:
https://hdl.handle.net/20.500.11824/1627
RT Journal T1
Aeroacoustic Analysis of a Closely Installed Chevron Nozzle Jet using the High-Order Discontinuous Galerkin Method
UL https://suche.suub.uni-bremen.de/peid=base-ftbcam:oai:bird.bcamath.org:20.500.11824_1627&Exemplar=1&LAN=DE A1 Lindblad, D A1 Sherwin, S A1 Cantwell, C A1 Lawrence, J A1 Proença, A A1 Moragues, M YR 2023 K1 Chevron Nozzles K1 Roe Approximate Riemann Solver K1 Ffowcs Williams Hawkings Equation K1 Large Eddy Simulation K1 Navier Stokes Equations K1 Power Spectral Density K1 Laminar to Turbulent Transition K1 Acoustic Mach Number K1 Stagnation Temperature K1 Aircraft Noise JF https://arc.aiaa.org/doi/abs/10.2514/6.2023-3831 LK http://dx.doi.org/https://hdl.handle.net/20.500.11824/1627 DO https://hdl.handle.net/20.500.11824/1627 SF ELIB - SuUB Bremen
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