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Experimental Study into the Flow Physics of Three-Dimensional Shock Control

View more insights in Professional - Physics - Engineering - Aeronautics - Natural Sciences

View more figures from Imperial College London

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This interview describes a fundamental experimental study of the flow structure around a single three-dimensional (3-D) transonic shock control bump (SCB) mounted on a flat surface in a wind tunnel.

Image courtesy of interviewee. November 28, 2016

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