{"_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", "sets": ["322"]}, "author_link": ["38031", "38032", "38033", "38034", "38035", "38036"], "item_10_alternative_title_19": {"attribute_name": "その他のタイトル", "attribute_value_mlt": [{"subitem_alternative_title": "Aerodynamic Interaction between Delta Wing and Hemisphere-Cylinder in Supersonic Flow", "subitem_alternative_title_language": "en"}]}, "item_10_biblio_info_6": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2005-10-05", "bibliographicIssueDateType": "Issued"}, "bibliographicIssueNumber": "621", "bibliographicPageEnd": "451", "bibliographicPageStart": "446", "bibliographicVolumeNumber": "53", "bibliographic_titles": [{"bibliographic_title": "日本航空宇宙学会論文集", "bibliographic_titleLang": "ja"}]}]}, "item_10_description_4": {"attribute_name": "抄録", "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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