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      Similarities Between Cellular Patterns Occurring in Transonic Buffet and Subsonic Stall

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          Abstract

          This paper studies the similarities between the three-dimensional (3-D) cellular patterns that appear in conditions of transonic buffet and subsonic stall, using Reynolds-averaged Navier–Stokes/unsteady Reynolds-averaged Navier–Stokes simulations. The geometries are obtained from the extrusion of a two-dimensional (2-D) airfoil with an added sweep angle, and periodic boundary conditions are imposed at both ends. First, numerical simulations of transonic buffet are performed. The numerical solutions exhibit three-dimensional cellular flow patterns, forming what has been named buffet cells. The latter are convected in the spanwise direction when a sweep angle is added, leading to the superposition of two frequencies. The first one is independent of the sweep angle and is characteristic of the two-dimensional buffet. The second one increases with the sweep angle and is related to the convection of the buffet cells. These cells are reminiscent of the stall cells, which are well known for low-speed flow conditions. Second, solutions of the unsteady Reynolds-averaged Navier–Stokes equations for infinite swept wings in stall conditions at low speed are computed, showing the same convection of the cellular patterns. These results indicate that the discrepancies between 2-D and 3-D buffet are caused by the appearance of stall cells, which are the same as buffet cells.

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                Author and article information

                Conference
                aiaaj
                AIAA Journal
                AIAA Journal
                American Institute of Aeronautics and Astronautics
                1533-385X
                18 September 2019
                January 2020
                : 58
                : 1
                : 71-84
                Affiliations
                ONERA-Paris Saclay University , 92190 Meudon, France
                Montreal Polytechnic , Montréal, Québec H3T 1J4, Canada
                Author notes
                [*]

                Ph.D. Student, Department of Aerodynamics, Aeroelasticity and Acoustics, 8 rue des Vertugadins; frederic.plante@ 123456polymtl.ca . Student Member AIAA.

                [†]

                Research Engineer, Department of Aerodynamics, Aeroelasticity and Acoustics, 8 rue des Vertugadins; julien.dandois@ 123456onera.fr .

                [‡]

                Professor, Department of Mechanical Engineering; eric.laurendeau@ 123456polymtl.ca . Member AIAA.

                Article
                J058555 J058555
                10.2514/1.J058555
                b6d37c84-fde1-4a6a-a89d-2f40380717b9
                Copyright © 2019 by the authors. 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 eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.
                History
                : 8 April 2019
                : 26 July 2019
                : 28 July 2019
                Page count
                Figures: 27, Tables: 2
                Funding
                Funded by: Natural Sciences and Engineering Research Council of Canada10.13039/501100000038
                Categories
                Regular Articles

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

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