Parametric study of compressible turbulent spots
JA Redford, ND Sandham, GT Roberts - … , held at the University of Trieste …, 2010 - Springer
JA Redford, ND Sandham, GT Roberts
Direct and Large-Eddy Simulation VII: Proceedings of the Seventh International …, 2010•SpringerAbstract The compressible Navier–Stokes equations are solved for turbulent spots at Mach 3
and 6, with both adiabatic and cold (T w= T∞) wall boundary conditions on a flat plate. From
the results turbulent spot growth and propagation rates are derived which will help to
quantify the length of laminar to turbulent transition. The simulations also yield skin-friction
and heat-transfer data.
and 6, with both adiabatic and cold (T w= T∞) wall boundary conditions on a flat plate. From
the results turbulent spot growth and propagation rates are derived which will help to
quantify the length of laminar to turbulent transition. The simulations also yield skin-friction
and heat-transfer data.
Abstract
The compressible Navier–Stokes equations are solved for turbulent spots at Mach 3 and 6, with both adiabatic and cold (T w = T ∞ ) wall boundary conditions on a flat plate. From the results turbulent spot growth and propagation rates are derived which will help to quantify the length of laminar to turbulent transition. The simulations also yield skin-friction and heat-transfer data.
Springer
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