{"created":"2023-06-20T15:11:38.762889+00:00","id":41336,"links":{},"metadata":{"_buckets":{"deposit":"9cd32825-dfcf-4e38-bc7b-ced32a9e3707"},"_deposit":{"created_by":1,"id":"41336","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41336"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041336","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["489541","489539","489540","489538"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical simulation of transonic flows about HOPE for high-speed flight demonstration"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"192","bibliographicPageStart":"187","bibliographicVolumeNumber":"46","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_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 7-9 Jun. 2000 東京 日本","subitem_description_type":"Other"}]},"item_3_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 7-9 Jun. 2000 Tokyo Japan","subitem_description_type":"Other"}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"無人往還機HOPE-X(宇宙往還技術機)の遷音速空力特性を調べるための高速飛行実証プログラムを計画した。この計画で使用される飛行実証機には、機首先端にADS(空気データシステム)のためのピトーブームが取り付けられた。この計画の準備として、ピトーブームの空力的影響を評価するために、この飛行実証機周囲の遷音速流の数値シミュレーションを行った。ここで使用したCFD(計算流体力学)コードは風上TVD(全変動減少)スキームを適用したFVM法(有限体積法)を使って差分化した、レイノルズ数平均化ナビエ-ストークス方程式に基づいている。ここで使用した計算格子は、4個のブロックからなるマルチブロック構造格子で、格子点の総数は約60万である。CFDシミュレーションの結果はピトーブームの空力的影響が非常に小さいことを示している。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A high-speed flight demonstration program has been planned to investigate transonic aerodynamic characteristics of the HOPE-X (H-2 Orbiting Plane-Experimental) unmanned re-entry vehicle. The flight demonstrator used in this program has a Pitot-boom for ADS (Air Data System) on its nose-tip. As a preparation for this program, numerical simulations of transonic flows about this flight demonstrator were executed in order to estimate the aerodynamic effect of the Pitot-boom. The CFD (Computational Fluid Dynamics) code used here is based on Reynolds averaged Navier-Stokes equations discretized using an FVM (Finite Volume Method) with a TVD (Total Variation Diminishing) upwind scheme. The computational grids used here are multi-block structured ones consisting of four blocks. Total number of the grid-points is about 0.6 millions. The CFD results show that the aerodynamic effect of Pitot-boom is very small.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028635035","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL SP-46","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_3_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_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"大興電子通信"},{"subitem_text_value":"航空宇宙技術研究所"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Daiko Denshi Tsushin Ltd"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"伊藤, 良三"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山本, 行光"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ito, Ryozo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Yukimitsu","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":"nalsp0046035.pdf","filesize":[{"value":"4.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0046035.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41336/files/nalsp0046035.pdf"},"version_id":"24361da7-57f2-4f74-b29f-81996db6991e"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"飛行実証計画","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速空力学","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE-X","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙往還技術試験機","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行実証機","subitem_subject_scheme":"Other"},{"subitem_subject":"ピトーブーム","subitem_subject_scheme":"Other"},{"subitem_subject":"全変動減少風上差分スキーム","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速流","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ-ストークス方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"TVD風上差分スキーム","subitem_subject_scheme":"Other"},{"subitem_subject":"レイノルズ数平均","subitem_subject_scheme":"Other"},{"subitem_subject":"FVM","subitem_subject_scheme":"Other"},{"subitem_subject":"有限体積法","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"flight demonstration program","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic aerodynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE X","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"H 2 Orbiting Plane Experimental","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight demonstrator","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Pitot boom","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"total variation diminishing upwind scheme","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"TVD upwind scheme","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Reynolds average","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"FVM","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"finite volume method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"HOPE高速飛行実証機の遷音速流解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"HOPE高速飛行実証機の遷音速流解析"}]},"item_type_id":"3","owner":"1","path":["1893","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"41336","relation_version_is_last":true,"title":["HOPE高速飛行実証機の遷音速流解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:02:50.796882+00:00"}