{"created":"2023-06-20T15:02:27.008928+00:00","id":31533,"links":{},"metadata":{"_buckets":{"deposit":"4219288e-339b-4dd2-a2d6-f3722e4c008e"},"_deposit":{"created_by":1,"id":"31533","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"31533"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00031533","sets":["1887:1890","1896:1898:1899:1910"]},"author_link":["404724","404725","404727","404726"],"item_9_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerically-Experimental Study on the Combustion and Performance of a Spark-Ignition Engine 4 Cycle Engine"}]},"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1974-10","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"4_A","bibliographicPageEnd":"767","bibliographicPageStart":"715","bibliographicVolumeNumber":"10","bibliographic_titles":[{"bibliographic_title":"東京大学宇宙航空研究所報告"}]}]},"item_9_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"どのような運転条件に対しても広く適用できるように数式化された燃焼速度をもとにし,燃焼室内の火炎伝播過程の一次元的数式モデルをつくり,更に断熱シリンダだけでなく,シリンダ壁との熱交換も考慮して,火花点火機関の燃焼過程と性能およびNO排出量に関する数値実験的研究を行った。今回は燃焼過程の数値実験的手法の確立に重きをおいたので牧排気のガス交換過程には最も簡単な理想的指圧線図を仮定した。牧人新気としては正-オクタン・空気混合気を用い燃焼ガス組成にはCO, CO_2, H, H_2, H_2O, N, N_2, NO, O, O_2, OHの11成分を考慮し,NO以外は化学平衡論的,NOに関してはN濃度定常のZeldovich機構による化学反応速度論的に取扱った。運転条件としてはとりあえず夫々他の条件を一定の標準条件にして,圧縮比,牧気圧(充填効率),回転数,着火時期,新気空燃比(当量比),燃焼速度をかえエンジン性能とNO排出量の計算を行った。多様な運転条件の下での複雑な計算であるが,尚多くの仮定を含むことは云うまでもない。しかし実機実験よりは数値実験の運転条件は明確であいまいさが少く,また実根実験では観測困難なよう","subitem_description_type":"Abstract"}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The present work has involved digital computer analysis of the performance of a spark ignition engine and the subsequent formation of the atmospheric pollutant NO by presenting a better understanding of the combustion process based on the onedimensional theory of flame propagation under the heat exchanging between walls and gas in the cylinder. Because of major interest in the combustion process for the presentation of a numerical simulation model, the gas exchange process is simply assumed to be of the idealized indicator diagram. As the fuel, n-octane and as the components of the burned gas, eleven species, CO, CO_2, H, H_2, H_2O, N, N_2, NO, O, O_2 and OH are considered to be in chemical equilibrium except for NO whose formation is predicted by Zeldovich mechanism. Stepwise solutions of the time- and space-dependent mass- and energy-conservation equations together with associated gasdynamic and chemical equations yield the time histories of thermodynamic properties and chemical compositions throughout the engine cycle under various operation conditions of the compression-ratio, the boost pressure (charging efficiency), the engine speed, the ignition timing, the air-fuel ratio (equivalence ratio), the burning velocity etc. The results demonstrate definitely major effects of these operating parameters on the cycle performance and provide comprehensibly the details of the combustion process and the NO formation during the engine operation, although the used assumptions still remain to be further investigated.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0124446000","subitem_description_type":"Other"}]},"item_9_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"東京大学宇宙航空研究所"}]},"item_9_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0563-8100","subitem_source_identifier_type":"ISSN"}]},"item_9_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00161914","subitem_source_identifier_type":"NCID"}]},"item_9_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東京大学宇宙航空研究所"},{"subitem_text_value":"東京大学宇宙航空研究所"}]},"item_9_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Aeroautical Science University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Aeroautical Science University of Tokyo"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"八田, 桂三"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"佐野, 妙子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"HATTA, Keizo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SANO, Taeko","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":"2020-01-23"}],"displaytype":"detail","filename":"SA0124446.pdf","filesize":[{"value":"2.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0124446.pdf","url":"https://jaxa.repo.nii.ac.jp/record/31533/files/SA0124446.pdf"},"version_id":"4a4d40d4-ea1a-4efc-9d1f-81563bd71970"}]},"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":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"火花点火機関の燃焼および性能に関する数値実験的研究 : 第1報4サイクル機関","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"火花点火機関の燃焼および性能に関する数値実験的研究 : 第1報4サイクル機関"}]},"item_type_id":"9","owner":"1","path":["1890","1910"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"31533","relation_version_is_last":true,"title":["火花点火機関の燃焼および性能に関する数値実験的研究 : 第1報4サイクル機関"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:57:21.190284+00:00"}