{"_buckets": {"deposit": "e5367db9-b6a4-4f47-a698-1513e3ee854c"}, "_deposit": {"id": "11996", "owners": [], "pid": {"revision_id": 0, "type": "depid", "value": "11996"}, "status": "published"}, "_oai": {"id": "oai:nagoya.repo.nii.ac.jp:00011996"}, "item_10_alternative_title_19": {"attribute_name": "\u305d\u306e\u4ed6\u306e\u8a00\u8a9e\u306e\u30bf\u30a4\u30c8\u30eb", "attribute_value_mlt": [{"subitem_alternative_title": "Investigation on Hypersonic Shock Interacting and Boundary-Layer Separating Flowfield around Two-Stage-To-Orbit Vehicle"}]}, "item_10_biblio_info_6": {"attribute_name": "\u66f8\u8a8c\u60c5\u5831", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2008-06-05", "bibliographicIssueDateType": "Issued"}, "bibliographicIssueNumber": "653", "bibliographicPageEnd": "285", "bibliographicPageStart": "278", "bibliographicVolumeNumber": "56", "bibliographic_titles": [{"bibliographic_title": "\u65e5\u672c\u822a\u7a7a\u5b87\u5b99\u5b66\u4f1a\u8ad6\u6587\u96c6"}]}]}, "item_10_description_4": {"attribute_name": "\u6284\u9332", "attribute_value_mlt": [{"subitem_description": "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. 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