Wave packets and turbulent jet noise
P Jordan, T Colonius - Annual review of fluid mechanics, 2013 - annualreviews.org
Turbulent jet noise is a controversial fluid mechanical puzzle that has amused and
bewildered researchers for more than half a century. Whereas numerical simulations are …
bewildered researchers for more than half a century. Whereas numerical simulations are …
Recent advances in feature extraction techniques for high-speed flowfields
S Unnikrishnan - Progress in Aerospace Sciences, 2023 - Elsevier
Abstract Space–time scale-resolved diagnostic and computational campaigns routinely
produce high-fidelity multi-disciplinary truth-model quality datasets for complex …
produce high-fidelity multi-disciplinary truth-model quality datasets for complex …
Wavepackets in the velocity field of turbulent jets
We study the velocity fields of unforced, high Reynolds number, subsonic jets, issuing from
round nozzles with turbulent boundary layers. The objective of the study is to educe …
round nozzles with turbulent boundary layers. The objective of the study is to educe …
A shock-capturing methodology based on adaptative spatial filtering for high-order non-linear computations
A shock-capturing methodology is developed for non-linear computations using low-
dissipation schemes and centered finite differences. It consists in applying an adaptative …
dissipation schemes and centered finite differences. It consists in applying an adaptative …
Three-dimensional boundary conditions for direct and large-eddy simulation of compressible viscous flows
G Lodato, P Domingo, L Vervisch - Journal of computational physics, 2008 - Elsevier
Navier–Stokes characteristic boundary conditions (NSCBC) usually assume the flow to be
normal to the boundary plane. In this paper, NSCBC is extended to account for convection …
normal to the boundary plane. In this paper, NSCBC is extended to account for convection …
Influence of nozzle-exit boundary-layer conditions on the flow and acoustic fields of initially laminar jets
Round jets originating from a pipe nozzle are computed by large-eddy simulations (LES) to
investigate the effects of the nozzle-exit conditions on the flow and sound fields of initially …
investigate the effects of the nozzle-exit conditions on the flow and sound fields of initially …
Influence of initial turbulence level on the flow and sound fields of a subsonic jet at a diameter-based Reynolds number of 105
Five isothermal round jets at Mach number and Reynolds number originating from a pipe
nozzle are computed by large-eddy simulations to investigate the effects of initial turbulence …
nozzle are computed by large-eddy simulations to investigate the effects of initial turbulence …
Large-eddy simulation of the flow and acoustic fields of a Reynolds number 105 subsonic jet with tripped exit boundary layers
Large-eddy simulations (LESs) of isothermal round jets at a Mach number of 0.9 and a
diameter-based Reynolds number Re D of 10 5 originating from a pipe are performed using …
diameter-based Reynolds number Re D of 10 5 originating from a pipe are performed using …
Antisymmetric oscillation modes in rectangular screeching jets
In this paper, the origin and the properties of the oscillation modes in screeching non-ideally
expanded rectangular jets are investigated using compressible implicit LES of rectangular …
expanded rectangular jets are investigated using compressible implicit LES of rectangular …
Turbulence and energy budget in a self-preserving round jet: direct evaluation using large eddy simulation
An axisymmetric jet at a diameter-based Reynolds number of 1.1× 104 is computed by a
large eddy simulation (LES) in order to investigate its self-similarity region. The LES …
large eddy simulation (LES) in order to investigate its self-similarity region. The LES …