{"created":"2023-06-20T15:08:21.036403+00:00","id":37775,"links":{},"metadata":{"_buckets":{"deposit":"68c37b1f-1c6f-44b0-8bdf-82ac0c33cfa6"},"_deposit":{"created_by":1,"id":"37775","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37775"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037775","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["482924","482922","482926","482925","482921","482923"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"A numerical simulation of nozzle flow of hypersonic wind tunnel"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"89","bibliographicPageStart":"85","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":"21世紀に向けて、スペースプレーンや超音速機の開発に用いる極超音速風洞のいくつかが建設中、あるいは計画されている。これらの風洞を設計するに当って、CFD(計算空気力学)技術を利用することが不可欠である。本論文は、極超音速風洞ノズル内流れの数値シミュレーションを述べる。T.J.Coakleyによるq-ω乱流モデルを利用した3次元ナビエ・ストークス方程式解法コードを用いて航空宇宙技術研究所(NAL)極超音速風洞に設置された出口マッハ数7.0の極超音速軸対称ノズルの中の流れを計算した。計算結果をNALで得られたノズル出口での流れの分布に関する実験データと比較し、妥当な一致をみた。また、断熱壁や等温壁などの壁面条件が出口流れに及ぼす効果を数値シミュレーションにより調べた。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Toward the 21th century, some hypersonic wind tunnels for development of space planes and supersonic transports are under construction and planned in Japan. For designing these wind tunnels, it is indispensable to make use of CFD (Computational Fluid Dynamics) technology. This paper describes a numerical simulation of the nozzle flow of a hypersonic wind tunnel. The flow through the hypersonic axisymmetric nozzle with exit Mach number 7.0, which was installed in the hypersonic wind tunnel of National Aerospace Laboratory (NAL), was calculated by using three dimensional Navier-Stokes codes with q - omega model of turbulence by T.J. Coakley. The calculated results were compared with the experimental data, which had also been obtained by NAL, on the flow distributions at nozzle exit. Comparison with experiment and calculation shows a reasonable agreement. The effect of wall conditions such as adiabatic wall or isothermal wall upon the exit flow distributions was also investigated by numerical simulation.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004171015","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":"川崎重工業 明石技術研究所"},{"subitem_text_value":"川崎重工業 明石技術研究所"},{"subitem_text_value":"川崎重工業 明石技術研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Kawasaki Heavy Industries Ltd Akashi Technical Institute"},{"subitem_text_language":"en","subitem_text_value":"Kawasaki Heavy Industries Ltd Akashi Technical Institute"},{"subitem_text_language":"en","subitem_text_value":"Kawasaki Heavy Industries Ltd Akashi Technical Institute"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"河嶋, 敬"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"吉田, 秀則"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"清瀬, 弘晃"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kawashima, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yoshida, Hidenori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kiyose, Hiromitsu","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":"nalsp0022014.pdf","filesize":[{"value":"348.6 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0022014.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37775/files/nalsp0022014.pdf"},"version_id":"7c711607-9eae-4737-9076-eb9eb729d6a4"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"極超音速ノズル","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ解析","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞ノズル","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速空気力学","subitem_subject_scheme":"Other"},{"subitem_subject":"内部流解析","subitem_subject_scheme":"Other"},{"subitem_subject":"ノズル出口流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"壁面温度条件","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":"CFD対風洞相関","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD応用","subitem_subject_scheme":"Other"},{"subitem_subject":"断熱壁条件","subitem_subject_scheme":"Other"},{"subitem_subject":"等温壁条件","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速軸対称ノズル","subitem_subject_scheme":"Other"},{"subitem_subject":"計算空気力学","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic nozzle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flow analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel nozzle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic aerodynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"internal flow analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nozzle exit flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wall thermal 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":"CFD wind tunnel correlation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD application","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"adiabatic wall condition","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"isothermal wall condition","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic axisymmetric nozzle","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":"極超音速風洞ノズルの流れの数値解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"極超音速風洞ノズルの流れの数値解析"}]},"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":"37775","relation_version_is_last":true,"title":["極超音速風洞ノズルの流れの数値解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:12:42.339540+00:00"}