Parametric study of compressible turbulent spots

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

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Southampton (e-Prints Soton)

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Last time updated on 05/04/2012

This paper was published in Southampton (e-Prints Soton).

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