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A novel hybrid numerical scheme with built-in hyperviscosity has been developed to address the accuracy and numerical instability in numerical simulation of isotropic compressible turbulence in a periodic domain at high turbulent Mach number.
The flame interaction with the jet turbulence is dominated by a cross-stream high turbulent transport mechanism; whereas, the interaction for the obstacle is driven by Kelvin–Helmholtz and Rayleigh Taylor instabilities.
High turbulent extent of water flow results in more uniform particle distribution in the horizontal tube.
This spurious high turbulent intensity in turn causes (i) a high turbulent viscosity to be applied, wrongly stabilizing the jet, and (ii) increased turbulent diffusion of heat, causing too deep and diffuse a stratification to be predicted.
Another theory is the one of dynamic capabilities, that is, the firm's capability to use its resources more adequately than others in a high turbulent environment.
An high turbulent flow environment is also confirmed by the formation of plunge pools, due to hydraulic jump, at the foresets-toesets transition.
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Increased levels of turbulence resulted in the expected higher turbulent burning velocities and flame front wrinkling.
Turbulence is significantly suppressed by gaseous combustion resulting in higher turbulent transport for the leaner mixtures, a successive push of the gaseous reaction zone towards the wall, incomplete combustion, and subsequent catalytic conversion of the leaked fuel.
Direct Numerical Simulation realizations were created of a temporal mixing layer in which combustion occurs under high-pressure (high-p) turbulent conditions.
A higher turbulent intensity leads to a higher turbulent burning velocity due to increased flame area, while the mean consumption speed remains close to the laminar flame speed.
Flames characterised by higher fuel gradients showed higher turbulent burning velocities.
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