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      Simultaneous Flowfield and Surface-Deflection Measurements of an Axisymmetric Jet and Adjacent Surface

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          Abstract

          The interaction of an underexpanded jet and a nearby adjacent compliant surface is considered in an effort to gain insight into the relevant fluid–structure interaction. High-quality simultaneous flowfield and surface-deflection data were obtained in this high-Reynolds-number flow using nonintrusive, full-field, optical diagnostics (planar particle image velocimetry and stereo/three-dimensional digital image correlation, respectively). Both experimental setups were rigorously validated in terms of their measurement resolution and accuracy, both individually and in a combined manner. The full-field surface deflection data indicate that the surface has a predominantly quasi-static response characterized by a “standing-wave” type contour along the jet axis. A large jetward deflection, on the order of 10 plate thicknesses, was observed near the first shock-cell region, which is consistent with previously obtained rigid-surface case surface pressure measurements. The compliant-surface flowfield was analyzed and compared to the rigid-surface case results in key regions: the initial expansion region, through the shock/boundary-layer interaction, the shock/boundary-layer interaction separation region, the shock-cell structure of the remainder of the jet plume, the near-wall boundary layer, and the far-field conditions. Notable differences were observed before, within, and after the shock/boundary-layer interaction region as well as within the boundary layer and in the shock-cell structure.

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          Most cited references39

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          Towards better uncertainty estimates for turbulence statistics

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            Shock Induced Fluid-Structure Interaction on a Flexible Wall in Supersonic Turbulent Flow

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              Unsteady fluid–structure interactions of membrane airfoils at low Reynolds numbers

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                Author and article information

                Journal
                aiaaj
                AIAA Journal
                AIAA Journal
                American Institute of Aeronautics and Astronautics
                0001-1452
                1533-385X
                27 October 2017
                March 2018
                : 56
                : 3
                : 917-932
                Affiliations
                University of Illinois at Urbana-Champaign , Urbana, Illinois 61801
                Author notes
                [*]

                Graduate Research Assistant, Aerospace Engineering, 104 South Wright Street. Student Member AIAA.

                [†]

                Professor, Aerospace Engineering, 104 South Wright Street. Associate Fellow AIAA.

                Article
                J056032 J056032
                10.2514/1.J056032
                c330e0dc-94d7-4360-b5fa-5f00a70cf75f
                Copyright © 2017 by Ruben Hortensius, J. Craig Dutton, and Gregory S. Elliott. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0001-1452 (print) or 1533-385X (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.
                History
                : 29 January 2017
                : 1 September 2017
                : 5 September 2017
                Page count
                Figures: 18, Tables: 2
                Funding
                Funded by: Army Research Office10.13039/100000183
                Award ID: W911NF-14-1-0404
                Categories
                Regular Article

                Engineering,Physics,Mechanical engineering,Space Physics
                Engineering, Physics, Mechanical engineering, Space Physics

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