{"created":"2023-06-20T15:08:20.987016+00:00","id":37774,"links":{},"metadata":{"_buckets":{"deposit":"b7c38238-8946-43a4-8d5a-340f0ecd81ff"},"_deposit":{"created_by":1,"id":"37774","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37774"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037774","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["482919","482916","482915","482918","482920","482917"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Dynamic and numerical simulations of restart phenomenon in scramjet intake"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"83","bibliographicPageStart":"79","bibliographicVolumeNumber":"22","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料: 第11回航空機計算空気力学シンポジウム論文集"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory: Proceedings of the 11th NAL Symposium on aircraft computational aerodynamics","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"航空宇宙技術研究所 10-11 Jun. 1993 東京 日本","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"National Aerospace Laboratory 10-11 Jun. 1993 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"スクラムジェット空気取入口モデルの内部の流れを陰的差分解法に基く2次元オイラー方程式の解によって数値的にシミュレートした。このシミュレーションを行うため、Chakravarthy-Osher型TVD(全変動減少型)定式化に基づいた数値解法を多段階格子法および移動格子法向きに改良した。スクラムジェットにおける不始動状態から回復する方法を研究するため、まず移動格子法を用いて定常状態から不始動状態までの動的な数値シミュレーションを行った。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The inner flow fields of scramjet intake model are simulated numerically by two dimensional Euler equations using an implicit finite difference scheme. For this simulations, the numerical scheme based on chakravarthy Osher's type TVD formulations is improved for both multi-grid and moving-grid application. To investigate the methods of recovery from unstart conditions in scramjet, at first, the dynamic and numerical simulations were conducted from steady condition to unstart condition using moving-grid.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004171014","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL SP-22","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"富士重工業"},{"subitem_text_value":"富士重工業"},{"subitem_text_value":"スバル研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Co Ltd"},{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Co Ltd"},{"subitem_text_language":"en","subitem_text_value":"Subaru Research Center Co Ltd"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"石川, 忠"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"若井, 洋"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山内, 豊誠"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishikawa, Tadashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Wakai, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamauchi, Toyosei","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0022013.pdf","filesize":[{"value":"449.3 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0022013.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37774/files/nalsp0022013.pdf"},"version_id":"1787cbed-c929-4d96-93ba-b36934a3bcdd"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"スクラムジェットエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"スクラムジェット空気取入口","subitem_subject_scheme":"Other"},{"subitem_subject":"空気取入口不始動","subitem_subject_scheme":"Other"},{"subitem_subject":"不始動回復法","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"オイラー方程式数値解","subitem_subject_scheme":"Other"},{"subitem_subject":"多段階格子法","subitem_subject_scheme":"Other"},{"subitem_subject":"移動境界法","subitem_subject_scheme":"Other"},{"subitem_subject":"動的流れシミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"内部流解析","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速内部流","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速推進機関","subitem_subject_scheme":"Other"},{"subitem_subject":"スペースプレーンエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"スクラムジェット流れ制御","subitem_subject_scheme":"Other"},{"subitem_subject":"scramjet engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"scramjet intake","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"intake unstart","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"unstart recovery","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical flow simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Euler equation numerical solution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"multigrid method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"moving boundary technique","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"dynamic flow simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"internal flow analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic internal flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic propulsion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spaceplane engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"scramjet flow control","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"jpn"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"スクラムジェットインテークの動的な再始動現象の数値計算","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"スクラムジェットインテークの動的な再始動現象の数値計算"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"37774","relation_version_is_last":true,"title":["スクラムジェットインテークの動的な再始動現象の数値計算"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:12:44.159343+00:00"}