{"created":"2023-06-20T15:11:38.810343+00:00","id":41337,"links":{},"metadata":{"_buckets":{"deposit":"3076d4f3-3f08-4ccf-8450-556690ca9aa4"},"_deposit":{"created_by":1,"id":"41337","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41337"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041337","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["489545","489542","489544","489543"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"CFD design study of HOPE-X aerodynamic characteristics"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"206","bibliographicPageStart":"193","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":"新しいHOPE(H-2ロケット打上げ型有翼回収機)11モデルの空力特性に関する数値解析を行った。本研究では総計約300例のCFD(計算流体力学)計算を実行した。亜/遷/超音速領域についてマッハ数0.4から3.0、迎角0度から20度、そして横すべり効果がある場合とない場合についてパラメトリックなマルチブロックのナビエ-ストークス(N-S)解析を実施した。遷音速流に関しては、マッハ数0.9と1.1でスティング干渉効果についても調べた。打ち上げ時の低超音速で低迎角の場合、乱流加熱のあることが予言されているが、数値計算の結果をAEDC(アーノルド技術開発センター)-HWT(極超音速風洞)実験と比較した。超音速再突入時の基本的な空力特性、空熱力学特性も、マッハ数0.8から26の範囲で、迎角30度、40度、50度の場合について調べた。この際、ボディフラップおよびエレボンの偏向などの舵面効き特性の検討を行った。実在気体効果は7化学種の非平衡1温度N-Sコードを使って解析した。全体的空力特性に対する化学反応の寄与を分割するため、3種類の異る気体モデル(完全気体、凍結流、実在気体モデル)を使った計算を実施した。これらのパラメトリック計算を通して、新しいHOPE11基本設計モデルの全体的な空力特性、空力加熱特性を評価した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Numerical study of aerodynamic characteristics of new HOPE (H-2 Orbiting Plane) 11 model is performed. In the present study, totally about 300 CFD (Computational Fluid Dynamics) calculations are carried out. For subsonic, transonic and supersonic speed range, parametric multi-block Navier-Stokes (N-S) analysis has been conducted from M(sub infinity) = 0.4 to 3.0 at angles of attack from 0 to 20 deg, with and without side slip effects. For transonic flows, sting interference effects are also investigated at M(sub infinity) = 0.9 and 1.1. Turbulent heating at low hypersonic speed in launching phase is predicted at low angles of attack and the numerical results are compared with AEDC (Arnolds Engineering Development Center) HWT (Hypersonic Wind Tunnel) experiments. Basic aero- and aerothermodynamic characteristics at hypersonic re-entry phase are also investigated from M(sub infinity) = 0.8 to M(sub infinity) = 26 at angles of attack alpha = 30 deg, 40 deg, and 50 deg, where the efficiency of control surface such as body flaps and elevon deflections is also studied. Real gas effects are analyzed by using a seven species chemically non-equilibrium one temperature N-S code. In order to divide contributions of chemical reactions to total aerodynamic performance, calculations using three different kind of gas models (perfect, frozen and real gas model) have been made. Through these parametric computations, total aero- and aerothermodynamic characteristics of new HOPE 11 basic design model are evaluated.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028635036","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":"航空宇宙技術研究所"},{"subitem_text_value":"大興電子通信"}]},"item_3_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":"Daiko Denshi Tsushin Ltd"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"山本, 行光"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"伊藤, 良三"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Yukimitsu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ito, Ryozo","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":"nalsp0046036.pdf","filesize":[{"value":"5.9 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0046036.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41337/files/nalsp0046036.pdf"},"version_id":"64c8f5aa-92a8-4529-969c-472088b25c8f"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"HOPE11","subitem_subject_scheme":"Other"},{"subitem_subject":"H-2ロケット打上げ型有翼回収機","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ-ストークス解析","subitem_subject_scheme":"Other"},{"subitem_subject":"空熱力学特性","subitem_subject_scheme":"Other"},{"subitem_subject":"横すべり効果","subitem_subject_scheme":"Other"},{"subitem_subject":"アーノルド技術開発センター","subitem_subject_scheme":"Other"},{"subitem_subject":"乱流加熱","subitem_subject_scheme":"Other"},{"subitem_subject":"AEDC-HWT実験","subitem_subject_scheme":"Other"},{"subitem_subject":"ボディフラップ","subitem_subject_scheme":"Other"},{"subitem_subject":"エレボン","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":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE 11","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"H 2 Orbiting Plane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerothermodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"side slip effect","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Arnold Engineering Development Center","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"turbulent heating","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"AEDC HWT experiment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"body flap","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"elevon","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"},{"subitem_subject":"numerical analysis","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の空力設計解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"HOPEの空力設計解析"}]},"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":"41337","relation_version_is_last":true,"title":["HOPEの空力設計解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:02:49.841976+00:00"}