{"_buckets": {"deposit": "9ce26b17-bc05-47a5-bc5a-d258fb00e96f"}, "_deposit": {"id": "12004", "owners": [], "pid": {"revision_id": 0, "type": "depid", "value": "12004"}, "status": "published"}, "_oai": {"id": "oai:nagoya.repo.nii.ac.jp:00012004"}, "item_10_alternative_title_19": {"attribute_name": "\u305d\u306e\u4ed6\u306e\u8a00\u8a9e\u306e\u30bf\u30a4\u30c8\u30eb", "attribute_value_mlt": [{"subitem_alternative_title": "Aerodynamic Interaction between Delta Wing and Hemisphere-Cylinder in Supersonic Flow"}]}, "item_10_biblio_info_6": {"attribute_name": "\u66f8\u8a8c\u60c5\u5831", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2005-10-05", "bibliographicIssueDateType": "Issued"}, "bibliographicIssueNumber": "621", "bibliographicPageEnd": "451", "bibliographicPageStart": "446", "bibliographicVolumeNumber": "53", "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": "As future space vehicles, Reusable Launch Vehicle (RLV) needs to be developed, where there are two kinds of RLV: Single Stage To Orbit (SSTO) and Two Stage To Orbit (TSTO). In the latter case, the shock/shock interaction and shock/boundary layer interaction play a key role. In the present study, we focus on the supersonic flow field with aerodynamic interaction between a delta wing and a hemisphere-cylinder, which imitate a TSTO, where the clearance, h, between the delta wing and hemisphere-cylinder is a key parameter. 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