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      Evaluating Dynamic Stall-Onset Criteria for Mixed and Trailing-Edge Stall

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          Abstract

          We evaluate two leading-edge-based dynamic stall-onset criteria (namely, the maximum magnitudes of the leading-edge suction parameter and the boundary enstrophy flux) for mixed and trailing-edge stall. These criteria have been shown to successfully predict the onset of leading-edge stall at Reynolds numbers of O ( 10 5 ) , where the leading-edge suction drops abruptly. However, for mixed/trailing-edge stall, leading-edge suction tends to persist even when there is significant trailing-edge reversed flow and stall is underway, necessitating further investigation into the effectiveness of these criteria. Using wall-resolved large-eddy simulations and the unsteady Reynolds-averaged Navier–Stokes method, we simulate one leading-edge stall and three mixed/trailing-edge stall cases at Reynolds numbers of 2 × 10 5 and 3 × 10 6 . We contrast the progression of flow features such as trailing-edge separation and vortex formation across different stall types and evaluate the stall-onset criteria relative to critical points in the flow. We find that the criteria nearly coincide with the instance of leading-edge suction collapse and are reached in advance of dynamic stall vortex formation and lift stall for all four cases. We conclude that the two criteria effectively signal dynamic stall onset in cases where the dynamic stall vortex plays a prominent role.

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          Most cited references39

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          A one-equation turbulence model for aerodynamic flows

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                Author and article information

                Contributors
                Conference
                aiaaj
                AIAA Journal
                AIAA Journal
                American Institute of Aeronautics and Astronautics
                1533-385X
                29 December 2022
                March 2023
                : 61
                : 3
                : 1181-1196
                Affiliations
                Iowa State University , Ames, Iowa 50011
                Mississippi State University , Mississippi State, Mississippi 39762
                Iowa State University , Ames, Iowa 50011
                Author notes
                [*]

                Graduate Student, Department of Aerospace Engineering.

                [†]

                Assistant Professor, Department of Aerospace Engineering. Senior Member AIAA.

                [‡]

                Associate Professor, Department of Aerospace Engineering. Associate Fellow AIAA.

                Author information
                https://orcid.org/0000-0003-4595-3852
                https://orcid.org/0000-0002-1768-8230
                https://orcid.org/0000-0002-8198-3891
                Article
                J062011 J062011
                10.2514/1.J062011
                ee2e3a80-1f10-4e9a-acd4-ff092bb8d5fd
                Copyright © 2022 by Sarasija Sudharsan and Anupam Sharma. 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
                : 08 June 2022
                : 13 October 2022
                : 19 November 2022
                Page count
                Figures: 23, Tables: 5
                Funding
                Funded by: National Science Foundationhttp://dx.doi.org/10.13039/100000001
                Award ID: CBET-1554196
                Award ID: CBET-1935255
                Award ID: XSEDE #TG-CTS130004
                Categories
                p2263, Fluid Dynamics
                p3624, Unsteady Aerodynamics
                p1804, Aerodynamics
                p2228, Aerospace Sciences
                p2073, Aeronautics
                Regular Articles

                Engineering,Physics,Mechanical engineering,Space Physics
                Stall onset criteria,Unsteady flow separation,Dynamic Stall,Unsteady Aerodynamics

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