Transonic shock/boundary layer interactions subject to downstream pressure perturbations

In the present study, an experimental investigation into the response of transonic SBLIs to periodic downstream pressure perturbations in a parallel walled duct has been conducted. Tests have been carried out for shock strengths of M<sub>∞</sub> = 1.4 and 1.5 with pressure perturbation f...

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Bibliographic Details
Main Author: Bruce, P. J. K.
Published: University of Cambridge 2009
Subjects:
Online Access:http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.597030