Abstract:V ERMA and Gupta 1 recently presented experimental data for the supersonic turbulent¯ow past a circular cylinder mounted on a¯at plate at a freestream Mach number of M = 1.6. Using their oil¯ow visualization data, Verma and Gupta 1 made an attempt to correlate the primary separation distance S with the cylinder diameter D and the thickness of the undisturbed boundary-layer d .Reference 1 concludedthat the appropriatelength scale for the separation distance is S/ p ( Dd ) (for H > d ) and proposed the following… Show more
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