{"created":"2023-06-20T15:07:30.428888+00:00","id":36874,"links":{},"metadata":{"_buckets":{"deposit":"0cf56add-7088-4b88-8076-69da0f25cc9f"},"_deposit":{"created_by":1,"id":"36874","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"36874"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00036874","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["477952","477951"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Effects of wall catalysis on the non-equilibrium hypersonic flow around reentry vehicle"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1997-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"82","bibliographicPageStart":"77","bibliographicVolumeNumber":"34","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_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 6-7 JUN. 1996 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 6-7 JUN. 1996 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"再突入物体周りの極超音速非平衡流れに及ぼす壁面触媒性の影響を非平衡効果を考慮した全ナビエ・ストークス方程式を解いて論じた。化学的、熱的非平衡効果を有する軸対称完全ナビエ・ストークス方程式をParkの2温度モデルとSSH(Schwartz-Slawsky-Herzfeld)理論からの振動緩和モデルを用いて考察した。時間積分については、LU-SGS(対称ガウス・ザイデル)スキームとソース項ヤコビ行列のための陰的対角法を組合わせた陰的差分法の有効数値アルゴリズムを用いた。対流項については、AUSMDVスキームを非平衡流の場合に一般化して適用した。OREX(軌道再突入実験機)周りの壁面の空力加熱率へ及ぼす触媒効率の影響を詳細に調べた。数種の飛行高度に対して数値解析を行い、飛行データと比較した。よどみ点における材料の触媒効率を推定し、スペースシャトルのような他の飛行物体の類似材料のデータとよく一致することを明らかにした。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Effects of surface catalysis on the nonequilibrium hypersonic flow around reentry vehicle are discussed by solving Navier-Stokes equations considering nonequilibrium effects. Axisymmetric full Navier-Stokes equations which have chemically and thermally nonequilibrium effects are considered by using Parks two-temperature model and the vibrational relaxation model from the SSH (Schwartz-Slawsky-Herzfeld) theory. For the time integration, an efficient numerical algorithm of an implicit finite difference method is used, which consists of the combination of LU-SGS (Lower-Upper Symmteric Gauss Seidel) scheme and the implicit diagonal method for a source Jacobian matrix. For convective terms, AUSMDV (Advection Upstream Splitting Method, mixture of flux Difference biased scheme and flux Vector biased scheme) scheme generalized into the nonequilibrium flow case is applied. Effects of catalytic efficiency on aerodynamic heating rates at the wall around OREX (Orbital Reentry Experiment) are examined in detail. Numerical analyzes are performed at several flight altitudes and compared with flight data. Catalytic efficiency of material at the stagnation point is estimated and it is clear that it shows good agreement with data of similar materials of another vehicles such as space shuttle.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000685015","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-34","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":"三菱電機 鎌倉製作所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Electric Corporation Kamakura Works"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"黒滝, 卓司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kurotaki, Takuji","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":"nalsp0034015.pdf","filesize":[{"value":"626.2 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0034015.pdf","url":"https://jaxa.repo.nii.ac.jp/record/36874/files/nalsp0034015.pdf"},"version_id":"368725a9-f127-4c05-9b4f-b6558dcbd241"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"再突入機","subitem_subject_scheme":"Other"},{"subitem_subject":"壁面触媒性","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速非平衡流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"軸対称ナビエ・ストークス方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"非平衡効果","subitem_subject_scheme":"Other"},{"subitem_subject":"Parkの2温度モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"振動緩和モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"陰的差分法","subitem_subject_scheme":"Other"},{"subitem_subject":"よどみ点","subitem_subject_scheme":"Other"},{"subitem_subject":"触媒効率","subitem_subject_scheme":"Other"},{"subitem_subject":"空力加熱率","subitem_subject_scheme":"Other"},{"subitem_subject":"OREX","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道再突入実験機","subitem_subject_scheme":"Other"},{"subitem_subject":"reentering vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wall catalysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nonequilibrium hypersonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"axisymmetric Navier Stokes equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nonequilibrium effect","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Parks two temperature model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"vibrational relaxation model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"implicit finite difference method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stagnation point","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"catalytic efficiency","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic heating rate","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"OREX","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbital reentry experiment","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":"再突入物体周りの極超音速非平衡流れに及ぼす壁面触媒性の影響について","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"再突入物体周りの極超音速非平衡流れに及ぼす壁面触媒性の影響について"}]},"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":"36874","relation_version_is_last":true,"title":["再突入物体周りの極超音速非平衡流れに及ぼす壁面触媒性の影響について"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:30:06.757300+00:00"}