Computation of unsteady turbomachinery flows: Part 2—LES and hybrids
PG Tucker - Progress in Aerospace Sciences, 2011 - Elsevier
The choice of turbulence model can have a strong impact on results for many
turbomachinery zones. Palliative corrections to them and also transition modeling can have …
turbomachinery zones. Palliative corrections to them and also transition modeling can have …
Trends in turbomachinery turbulence treatments
PG Tucker - Progress in Aerospace Sciences, 2013 - Elsevier
General forms of turbulence models are outlined along with their defects and palliatives for
these in relation to turbomachinery. The turbulence modelling hierarchy available in …
these in relation to turbomachinery. The turbulence modelling hierarchy available in …
Establishing consensus turbulence statistics for hot subsonic jets
Several articles in the open literature document previous efforts to measure turbulent jets.
Most were acquired in cold, low speed jets, often using hotwire anemometry, although some …
Most were acquired in cold, low speed jets, often using hotwire anemometry, although some …
The NASA subsonic jet particle image velocimetry (PIV) dataset
Many tasks in fluids engineering require prediction of turbulence of jet flows. The present
document documents the single-point statistics of velocity, mean and variance, of cold and …
document documents the single-point statistics of velocity, mean and variance, of cold and …
Hybrid source model for predicting high-speed jet noise
SJ Leib, ME Goldstein - AIAA journal, 2011 - arc.aiaa.org
JET mixing noise continues to be the main contributor to overall aircraft noise on takeoff,
despite significant increases in engine bypass ratios. The development of effective mixing …
despite significant increases in engine bypass ratios. The development of effective mixing …
Simulations of initially highly disturbed jets with experiment-like exit boundary layers
Two isothermal round jets at a Mach number of 0.9 and a diameter-based Reynolds number
of 2× 10 5 have been computed by compressible large-eddy simulation using high-order …
of 2× 10 5 have been computed by compressible large-eddy simulation using high-order …
LES–RANS of installed ultra-high-bypass-ratio coaxial jet aeroacoustics with flight stream
Using large-eddy simulation–Reynolds-averaged Navier–Stokes (LES–RANS), this paper
studies a round coaxial nozzle with an ultra-high bypass ratio of 15, with and without a wing …
studies a round coaxial nozzle with an ultra-high bypass ratio of 15, with and without a wing …
Space-time correlation measurements in nearfields of jets
K Viswanathan, JR Underbrink, L Brusniak - AIAA journal, 2011 - arc.aiaa.org
Space–time correlation characteristics of jets operated over a wide range of jet velocities are
investigated in this study, in order to gain insights into the physical mechanisms that lead to …
investigated in this study, in order to gain insights into the physical mechanisms that lead to …
Computation of high-speed coaxial jets with fan flow deflection
THE coaxial jet with normal velocity profile hasflow features that can be controlled to reduce
sound in azimuthal directions of relevance to aircraft noise. To appreciate these features, let …
sound in azimuthal directions of relevance to aircraft noise. To appreciate these features, let …
Validating large-eddy simulation for jet aeroacoustics
TYPICAL aeroacoustic problems are bedeviled at several levels. First, thefluidflow
generating the acousticfield is turbulent, and the flow and its associated sound are …
generating the acousticfield is turbulent, and the flow and its associated sound are …