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document
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Alauzet, F. (author)
This paper presents an accurate approach to simulate the sonic boom of a supersonic aircraft. The near field flow is modeled by the conservative Euler equations and is solved using a finite volume approach on adapted unstructured tetrahedral meshes. Then, from the CFD solution, the pressure distribution under the aircraft is extracted and used...
conference paper 2006
Source URL (retrieved on 2024-06-01 15:09): https://repository.tudelft.nl/islandora/search/collection%3Aconference?collection=research&display=tud_default&f%5B0%5D=mods_subject_topic_ss%3A%22finite%5C%20volume%5C%20method%22&f%5B1%5D=mods_subject_topic_ss%3A%22mesh%5C%20adaptation%22