@article{oai:nagoya.repo.nii.ac.jp:00011996, author = {北村, 圭一 and KITAMURA, Keiichi and 小澤, 啓伺 and OZAWA, Hiroshi and 花井, 勝祥 and HANAI, Katsuhisa and 森, 浩一 and MORI, Koichi and 中村, 佳朗 and NAKAMURA, Yoshiaki}, issue = {653}, journal = {日本航空宇宙学会論文集}, month = {Jun}, note = {To explore future RLVs, a hypersonic flowfield around a Two-Stage-To-Orbit (TSTO) configuration is analyzed in this paper. This study also demonstrates how CFD, as a powerful tool, can be applied to investigate such a complex flowfield involving a shock/shock interaction and a boundary-layer separation. First, the hypersonic flow around two bodies of the TSTO model has been numerically simulated, and then, the results are validated by comparing with experimental data taken at the UT-Kashiwa Hypersonic Tunnel. Finally, the detailed, computed flowfield is shown to have pairs of streamwise vortices (including horseshoe vortices) with alternating signs of rotation around the TSTO body surfaces.}, pages = {278--285}, title = {極超音速TSTOにおける衝撃波干渉・境界層剥離を伴う流れ場の解析}, volume = {56}, year = {2008} }