2026-03-13T08:36:00Z https://fukuyama-u.repo.nii.ac.jp/oai

oai:fukuyama-u.repo.nii.ac.jp:00008115 2023-06-19T10:30:04Z 502:505:675:710

Investigation of Flowfield around Hypersonic Space Plane Investigation of Flowfield around Hypersonic Space Plane Space Plane Hypersonic Flow Electric Discharge Method Finite Element Method P(論文) The flowfield analysis around a model of space plane traveling at Mach 10 has been carried out utilizing the Electric Discharge Method and the Finite Element Method (FEM) scheme The Electric Discharge Method can be visualized almost all important hypersonic flowfield phenomena, such as three-dimensional shock shapes, streamlines near wall surface, distant streamlines from wall surface, and boundary layers etc. In this study, the experiments and the numerical simulations were carried out under the conditions the angles of attack were 0 and 10 deg. Furthermore, the experimental results were compared with the numerical ones. In these comparisons, it was found that they were relatively in good agreement. departmental bulletin paper 2002-12 application/pdf 福山大学工学部紀要 26 143 148 AN00217655 https://fukuyama-u.repo.nii.ac.jp/record/8115/files/KJ00005781500.pdf https://fukuyama-u.repo.nii.ac.jp/records/8115 eng