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Unsteady Aspects of Shock-Wave/Boundary-Layer Interaction Resulting from Control Surface Deflection
A computational investigation of a Mach 6.9 turbulent flow near the juncture (cove) of a wing’s trailing-edge and elevon was carried out. Turbulence was modeled using improved delayed detached eddy simulation (IDDES). The computational data were compared to the results of an experimental study, cond...
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Published in: | AIAA journal 2022-08, Vol.60 (8), p.4649-4659 |
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description | A computational investigation of a Mach 6.9 turbulent flow near the juncture (cove) of a wing’s trailing-edge and elevon was carried out. Turbulence was modeled using improved delayed detached eddy simulation (IDDES). The computational data were compared to the results of an experimental study, conducted by Deveikis and Bartlett, which simulated the flow over the windward surface of the NASA space shuttle. Flow visualization, surface variable comparison with experiment, and analysis of unsteady flow statistics were carried out. Reasonable agreement between prediction and measurement was obtained for time-averaged surface pressure and heat flux. Unsteady analysis of these quantities revealed spectra dominated by low-frequency energy content throughout the interaction region. A correlation analysis indicated coupling of the unsteady motions of the shear layer, shock wave, separation vortex, and flow reattachment. The results of the present study suggest that IDDES can be a valuable tool for the analysis of heating and unsteadiness in hypersonic gap flows. |
doi_str_mv | 10.2514/1.J061337 |
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Turbulence was modeled using improved delayed detached eddy simulation (IDDES). The computational data were compared to the results of an experimental study, conducted by Deveikis and Bartlett, which simulated the flow over the windward surface of the NASA space shuttle. Flow visualization, surface variable comparison with experiment, and analysis of unsteady flow statistics were carried out. Reasonable agreement between prediction and measurement was obtained for time-averaged surface pressure and heat flux. Unsteady analysis of these quantities revealed spectra dominated by low-frequency energy content throughout the interaction region. A correlation analysis indicated coupling of the unsteady motions of the shear layer, shock wave, separation vortex, and flow reattachment. The results of the present study suggest that IDDES can be a valuable tool for the analysis of heating and unsteadiness in hypersonic gap flows.</description><identifier>ISSN: 0001-1452</identifier><identifier>EISSN: 1533-385X</identifier><identifier>DOI: 10.2514/1.J061337</identifier><language>eng</language><publisher>Virginia: American Institute of Aeronautics and Astronautics</publisher><subject>Aeronautics ; Boundary conditions ; Boundary layer interaction ; Control surfaces ; Correlation analysis ; Detached eddy simulation ; Flow control ; Flow simulation ; Flow visualization ; Geometry ; Heat flux ; Pressure ; Reynolds number ; Shear layers ; Shock wave interaction ; Simulation ; Software ; Turbulence ; Unsteady flow ; Visualization</subject><ispartof>AIAA journal, 2022-08, Vol.60 (8), p.4649-4659</ispartof><rights>Copyright © 2022 by Robert Alviani, Jonathan Poggie, and Gregory Blaisdell. 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 ; employ the eISSN to initiate your request. See also AIAA Rights and Permissions .</rights><rights>Copyright © 2022 by Robert Alviani, Jonathan Poggie, and Gregory Blaisdell. 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. 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subjects | Aeronautics Boundary conditions Boundary layer interaction Control surfaces Correlation analysis Detached eddy simulation Flow control Flow simulation Flow visualization Geometry Heat flux Pressure Reynolds number Shear layers Shock wave interaction Simulation Software Turbulence Unsteady flow Visualization |
title | Unsteady Aspects of Shock-Wave/Boundary-Layer Interaction Resulting from Control Surface Deflection |
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