{"_buckets": {"deposit": "31f4e401-6e84-4a54-86e1-db062eac2bbc"}, "_deposit": {"created_by": 3, "id": "5053", "owners": [3], "pid": {"revision_id": 0, "type": "depid", "value": "5053"}, "status": "published"}, "_oai": {"id": "oai:ir.kagoshima-u.ac.jp:00005053", "sets": ["92"]}, "author_link": ["113706", "113711", "113705", "113701", "113702", "5359", "113708", "113710", "113707", "113703", "113704", "113709"], "item_6_alternative_title_18": {"attribute_name": "別言語のタイトル", "attribute_value_mlt": [{"subitem_alternative_title": "Numerical Calculation of Underexpanded Axisymmetric Supersonic Jet : Effects of Nozzle Divergence Angle and Mach Number on Shock Cell Length"}]}, "item_6_alternative_title_19": {"attribute_name": "タイトルよみ", "attribute_value_mlt": [{"subitem_alternative_title": "フソク ボウチョウ ジク タイショウ チョウ オンソク フンリュウ ノ スウチ ケイサン : ショック セル ナガサ ニ オヨボス ノズル ヒロガリカド ト マッハスウ ノ エイキョウ"}]}, "item_6_biblio_info_5": {"attribute_name": "収録雑誌名", "attribute_value_mlt": [{"bibliographicIssueNumber": "589", "bibliographicPageEnd": "3242", "bibliographicPageStart": "3236", "bibliographicVolumeNumber": "61", "bibliographic_titles": [{"bibliographic_title": "日本機械学會論文集. B編"}]}]}, "item_6_date_6": {"attribute_name": "作成日", "attribute_value_mlt": [{"subitem_date_issued_datetime": "1995-09-01"}]}, "item_6_description_4": {"attribute_name": "要約(Abstract)", "attribute_value_mlt": [{"subitem_description": "A numerical study of underexpanded axisymmetric supersonic jets is presented. The TVD finitedifference\nscheme is employed for the numerical calculation of Euler\u0027s equations. The numerical\nresults are compared both with results from the theoretical shock cell spacing formula suggested by\nTam and with previous experimental results. For nozzles having no divergence angle at the nozzle\nexit, a good agreement is obtained among the theoretical, experimental and numerical results for\npressure ratios across the nozzle until the occurrence of a Mach disk in the jet. For nozzles having\na divergence angle at the nozzle exit, the effects of the divergence angle, the nozzle design Mach\nnumber and the pressure ratio across the nozzle on the shock cell length are discussed and clarified.", "subitem_description_type": "Other"}]}, "item_6_full_name_2": {"attribute_name": "著者よみ", "attribute_value_mlt": [{"nameIdentifiers": [{"nameIdentifier": "113704", "nameIdentifierScheme": "WEKO"}], "names": [{"name": "カタノダ, ヒロシ"}]}, {"nameIdentifiers": [{"nameIdentifier": "113705", "nameIdentifierScheme": "WEKO"}], "names": [{"name": "ミヤザト, ヨシアキ"}]}, {"nameIdentifiers": [{"nameIdentifier": "113706", "nameIdentifierScheme": "WEKO"}], "names": [{"name": "マスダ, ミツハル"}]}, {"nameIdentifiers": [{"nameIdentifier": "113707", "nameIdentifierScheme": "WEKO"}], "names": [{"name": "マツオ, カズヤス"}]}]}, "item_6_full_name_3": {"attribute_name": "別言語の著者", "attribute_value_mlt": [{"nameIdentifiers": [{"nameIdentifier": "113708", "nameIdentifierScheme": "WEKO"}], "names": [{"name": "KATANODA, Hiroshi"}]}, {"nameIdentifiers": [{"nameIdentifier": "113709", "nameIdentifierScheme": "WEKO"}], "names": [{"name": "MIYAZATO, Yoshiaki"}]}, {"nameIdentifiers": [{"nameIdentifier": "113710", "nameIdentifierScheme": "WEKO"}], "names": [{"name": "MASUDA, Mitsuharu"}]}, {"nameIdentifiers": [{"nameIdentifier": "113711", "nameIdentifierScheme": "WEKO"}], "names": [{"name": "MATSUO, Kazuyasu"}]}]}, "item_6_publisher_23": {"attribute_name": "公開者・出版者", "attribute_value_mlt": [{"subitem_publisher": "日本機械学会"}]}, "item_6_relation_11": {"attribute_name": "DOI", "attribute_value_mlt": [{"subitem_relation_type": "isIdenticalTo", "subitem_relation_type_id": {"subitem_relation_type_id_text": "10.1299/kikaib.61.3236", "subitem_relation_type_select": "DOI"}}]}, "item_6_relation_32": {"attribute_name": "関連（relation）", "attribute_value_mlt": [{"subitem_relation_name": [{"subitem_relation_name_text": "http://joi.jlc.jst.go.jp/JST.Journalarchive/kikaib1979/61.3236"}]}]}, "item_6_rights_12": 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