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Nearfield anisotropic mesh adaptation for the third AIAA Sonic Boom Workshop
Sonic boom prediction is critical for the development of low-boom supersonic aircraft and encouraging a replacement of the overland commercial supersonic ban with a certification standard. The Third AIAA Sonic Boom Workshop nearfield test cases provide a unique opportunity to review anisotropic adap...
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Published in: | Journal of aircraft 2022 |
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container_title | Journal of aircraft |
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creator | Vanharen, Julien Loseille, Adrien Alauzet, Frédéric Park, Micheal Andrew |
description | Sonic boom prediction is critical for the development of low-boom supersonic aircraft and encouraging a replacement of the overland commercial supersonic ban with a certification standard. The Third AIAA Sonic Boom Workshop nearfield test cases provide a unique opportunity to review anisotropic adaptive-mesh strategies for complex geometries with important propulsion interaction effects. Anisotropic metrics formulated to control estimated Mach interpolation and integrated nearfield pressure signature (goal-oriented) errors are compared with the results obtained on workshop-provided meshes. Detailed flow solutions and mesh renderings are combined with computational Schlieren images to reveal the complex interactions present in a shock-plume interaction wind tunnel model and a prototype of the Low-Boom Flight Demonstrator. A favorable comparison of independent implementations of the entire simulation process provides evidence that each process is implemented correctly and sets a solid foundation for confidence in the nearfield prediction of each method. |
doi_str_mv | 10.2514/1.C036502 |
format | article |
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issn | 0021-8669 1533-3868 |
language | eng |
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source | Alma/SFX Local Collection |
subjects | Computational Physics Physics |
title | Nearfield anisotropic mesh adaptation for the third AIAA Sonic Boom Workshop |
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