Department of Mechanical and Aerospace Engineering
University of California, San Diego
Abstract-
In technological applications such as high-speed propulsion
and energetic devices, the variation in thermodynamic variables
associated with large heat release and/or high speeds
interacts with and
modifies the underlying turbulent flow. Direct numerical
simulations of the reacting shear layer
are performed over a wide
range of heat release rates and convective Mach numbers to quantify
and understand some of these modifications to the turbulence evolution
and structure.
Simulations are performed with up to 20 million grid
points, high-order discretization,
and with large evolution times
required to achieve full-blown turbulence.
The mixing rates and turbulence structure are found to be
substantially different with respect to the incompressible
case. DNS results and supporting analysis will be
presented to explain the observed compressibility effects.
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