{"created":"2023-06-20T15:08:21.183190+00:00","id":37778,"links":{},"metadata":{"_buckets":{"deposit":"e69aefae-eb53-4322-838a-8fb16f595274"},"_deposit":{"created_by":1,"id":"37778","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37778"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037778","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["482939","482943","482942","482946","482940","482941","482945","482944"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical analysis of scramjet nozzle flow: Under absence of reaction"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"108","bibliographicPageStart":"103","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":"Baldwin-Lomax代数渦粘性モデルを用いた3次元ナビエ・ストークス方程式とマルチブロック法により、スクラムジェットノズル内の窒素ガス非反応性流れを計算する数値手法を提案した。左右の側壁の後端が主流方向に対して直角でない場合を扱った。静圧、表面摩擦係数、熱流束、推力などノズル内流れの計算結果を周囲の条件の効果を入れない不足膨脹流れの場合について実験データと比較した。長さの異なる2つのノズルのいずれの場合もノズル推力につき2〜4％の不確かさで一致した。各種の周囲条件(マッハ数6の流れもしくは不足膨脹または過膨脹となる圧力の下にある静止気体)の下での計算によって得た流れ場についても調べた。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A proposal of numerical procedure is given for nonreacting flows of ideal N2 gas through scramjet nozzles by using a multi-grid method and the three dimensional Navier-Stokes equations with the Baldwin-Lomax algebraic eddy viscosity model. Here trailing edges of side-walls are assumed not to be perpendicular to a streamwise axis. The computational results of nozzle internal flow such as static pressure, skin friction coefficient, heat flux, thrust etc. are compared with experimental data for the under-expansion case with no effect of ambient condition. Both of them agree with uncertainties of two to four percent for the thrust of nozzle. Flowfields obtained by computations under various ambient conditions (flow of M(sub infinity) = six or still gas with pressure of under- or over-expansion) are also investigated.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004171018","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":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"石黒, 登美子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"高木, 亮治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"三谷, 徹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"平岩, 徹夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishiguro, Tomiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takaki, Ryoji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Mitani, Toru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hiraiwa, Tetsuo","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":"nalsp0022017.pdf","filesize":[{"value":"656.3 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0022017.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37778/files/nalsp0022017.pdf"},"version_id":"79be177c-20ec-4911-a8cd-cd42c64ac148"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"スクラムジェットノズル","subitem_subject_scheme":"Other"},{"subitem_subject":"スクラムジェットエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"推力計算","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速推進機関","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速非反応性流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速内部流解析","subitem_subject_scheme":"Other"},{"subitem_subject":"ノズル周囲条件","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークス方程式数値解","subitem_subject_scheme":"Other"},{"subitem_subject":"マルチブロック法","subitem_subject_scheme":"Other"},{"subitem_subject":"物体適合格子系","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD応用","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD対風洞相関","subitem_subject_scheme":"Other"},{"subitem_subject":"計算空気力学","subitem_subject_scheme":"Other"},{"subitem_subject":"scramjet nozzle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"scramjet engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thrust estimation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic propulsion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic nonreacting flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic internal flow analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nozzle ambient condition","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical flow simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equation numerical solution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"multiblock method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"body fitted grid system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD application","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD wind tunnel correlation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Computational Fluid Dynamics","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":"スクラムノズル流の数値解析:反応のない場合","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"スクラムノズル流の数値解析:反応のない場合"}]},"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":"37778","relation_version_is_last":true,"title":["スクラムノズル流の数値解析:反応のない場合"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:12:37.677523+00:00"}