{"_buckets": {"deposit": "b6778b84-8045-4f1d-b988-774043b23f6c"}, "_deposit": {"created_by": 1, "id": "44617", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "44617"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00044617", "sets": ["1893", "1917"]}, "author_link": ["470370", "470371", "470372", "470369"], "item_3_alternative_title_2": {"attribute_name": "その他のタイトル（英）", "attribute_value_mlt": [{"subitem_alternative_title": "Investigation of Air Stream from Combustor-Liner Air Entry Holes(III)"}]}, "item_3_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "1974-06", "bibliographicIssueDateType": "Issued"}, "bibliographicPageStart": "21", "bibliographicVolumeNumber": "369", "bibliographic_titles": [{"bibliographic_title": "航空宇宙技術研究所報告"}, {"bibliographic_title": "Technical Report of National Aerospace Laboratory TR-369", "bibliographic_titleLang": "en"}]}]}, "item_3_description_17": {"attribute_name": "抄録（英）", "attribute_value_mlt": [{"subitem_description": "Investigation of the jets flowing from air entry holes of the combustor liner of a gas turbine was carried out following the previous experiments using simplified models. Cold air was supplied through the air entry holes normally into the primary hot-gas flows. The mass flow of the primary hot-gas and issuing jets were measured, and the behavior of the air-jets was studied by the measurement of the temperature distribution of the gas mixture. The air-jets flowing from three circular air entry holes being parallel to the primary flow, single streamwise-long holes and two opposing circular holes were studied. The effects of jet and gas stream velocities and of gas temperature, together with these different configurations, were investigated. The discharge coefficient, the maximum penetration of the jets, the jet flow path, the mixing of the jets, and temperature distribution across the jets were investigated. Empirical expressions which describe the characteristics of the jets under the conditions of the experiments were formulated. The experimental results were compared with the results given by a standard circular hole and their characteristics were discussed.", "subitem_description_type": "Other"}]}, "item_3_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: NALTR0369000", "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 TR-369", "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": "0389-4010", "subitem_source_identifier_type": "ISSN"}]}, "item_3_text_34": {"attribute_name": "メタデータ提供者", "attribute_value_mlt": [{"subitem_text_value": "メタデータ提供者: NAL-MATCH"}]}, "item_3_text_35": {"attribute_name": "JAXAカテゴリ", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ: 航空宇宙技術研究所"}]}, "item_3_text_36": {"attribute_name": "JAXAカテゴリ2", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ2: AP"}]}, "item_3_text_43": {"attribute_name": "DSpaceコレクション番号", "attribute_value_mlt": [{"subitem_text_value": "DSpaceコレクション番号: 9"}]}, "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原動機部"}, {"subitem_text_value": "航空宇宙技術研究所原動機部"}]}, "item_3_text_7": {"attribute_name": "著者所属（英）", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Aeroengine Division, National Aerospace Laboratory(NAL)"}, {"subitem_text_language": "en", "subitem_text_value": "Aeroengine Division, National Aerospace Laboratory(NAL)"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "相波, 哲朗"}], "nameIdentifiers": [{"nameIdentifier": "470369", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "中野, 篤治"}], "nameIdentifiers": [{"nameIdentifier": "470370", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "AIBA, Tetsuro", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "470371", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "NAKANO, Tokuji", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "470372", "nameIdentifierScheme": "WEKO"}]}]}, "item_files": {"attribute_name": "ファイル情報", "attribute_type": "file", "attribute_value_mlt": [{"accessrole": "open_date", "date": [{"dateType": "Available", "dateValue": "2020-01-29"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "naltr00369.pdf", "filesize": [{"value": "2.5 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 2500000.0, "url": {"label": "naltr00369.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/44617/files/naltr00369.pdf"}, "version_id": "7e1bbee2-d791-482f-8571-d7f20f4043c5"}]}, "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": "高負荷燃焼器の空気孔からの流れについて(Ⅲ)", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "高負荷燃焼器の空気孔からの流れについて(Ⅲ)"}]}, "item_type_id": "3", "owner": "1", "path": ["1893", "1917"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/44617", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "44617", "relation": {}, "relation_version_is_last": true, "title": ["高負荷燃焼器の空気孔からの流れについて(Ⅲ)"], "weko_shared_id": -1}