WEKO3
アイテム
{"_buckets": {"deposit": "f3b9e370-2fa1-47ba-ae61-10d0e7a743f1"}, "_deposit": {"created_by": 1, "id": "43536", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "43536"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00043536", "sets": ["1893", "1915"]}, "author_link": ["464132", "464129", "464131", "464130"], "item_3_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Three Dimensional Calculation of Flow inside Supersonic Inlet"}]}, "item_3_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "1991-12", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "256", "bibliographicPageStart": "251", "bibliographicVolumeNumber": "16", "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 SP-16", "bibliographic_titleLang": "en"}]}]}, "item_3_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "A three dimensional Navier-Stokes calculation of flow inside a supersonic mixed-compression inlet, designed for Mach 2.5, was carried out. A multi-block method was applied to the calculation grids. Complex configurations of bleed holes and throat slot were simulated in order to compare the solution with experimental data. As a result, detail information of the flow, which was usually difficult to obtain in an experiment, was obtained. On this inlet under the supersonic flow through conditions, the flow was found to be two dimensional in 90% of spanwise direction. In the vicinity of the side-walls, however, three-dimensional separation occurred along the cowl shock. The separation induced a vortex, and the vortex was stretched and swallowed into the throat slot. The ramp bleed ahead of the cowl-shock-impinge line was found to play an important role for avoiding the separation region to spread. A static-wall-pressure comparison between the results and the experimental data showed reasonable agreement.", "subitem_description_type": "Other"}]}, "item_3_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: NALSP0016040", "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-16", "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_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": "川崎重工業株式会社岐阜技術研究所"}, {"subitem_text_value": "東北大学流体科学研究所"}]}, "item_3_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Gifu Technical Institute Kawasaki Heavy Industries, Ltd."}, {"subitem_text_language": "en", "subitem_text_value": "Institute of Fluid Science Tohoku University"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "藤本, 朗"}], "nameIdentifiers": [{"nameIdentifier": "464129", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "沢田, 恵介"}], "nameIdentifiers": [{"nameIdentifier": "464130", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Fujimoto, Akira", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "464131", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Sawada, Keisuke", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "464132", "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": "2020-01-28"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "nalsp0016040.pdf", "filesize": [{"value": "1.8 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 1800000.0, "url": {"label": "nalsp0016040.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/43536/files/nalsp0016040.pdf"}, "version_id": "c5b06673-a3a0-4d4d-91dd-59244c89c98e"}]}, "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": "超音速空気取入口内の流れについて", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "超音速空気取入口内の流れについて"}]}, "item_type_id": "3", "owner": "1", "path": ["1893", "1915"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/43536", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "43536", "relation": {}, "relation_version_is_last": true, "title": ["超音速空気取入口内の流れについて"], "weko_shared_id": -1}
超音速空気取入口内の流れについて
https://jaxa.repo.nii.ac.jp/records/43536
https://jaxa.repo.nii.ac.jp/records/43536bce3a83c-e830-4a36-91e9-6e56b812c74e
名前 / ファイル | ライセンス | アクション |
---|---|---|
nalsp0016040.pdf (1.8 MB)
|
|
Item type | テクニカルレポート / Technical Report(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 超音速空気取入口内の流れについて | |||||
言語 | ||||||
言語 | jpn | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Three Dimensional Calculation of Flow inside Supersonic Inlet | |||||
著者 |
藤本, 朗
× 藤本, 朗× 沢田, 恵介× Fujimoto, Akira× Sawada, Keisuke |
|||||
著者所属 | ||||||
川崎重工業株式会社岐阜技術研究所 | ||||||
著者所属 | ||||||
東北大学流体科学研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
Gifu Technical Institute Kawasaki Heavy Industries, Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Fluid Science Tohoku University | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory(NAL) | |||||
書誌情報 |
航空宇宙技術研究所特別資料 en : Special Publication of National Aerospace Laboratory SP-16 巻 16, p. 251-256, 発行日 1991-12 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A three dimensional Navier-Stokes calculation of flow inside a supersonic mixed-compression inlet, designed for Mach 2.5, was carried out. A multi-block method was applied to the calculation grids. Complex configurations of bleed holes and throat slot were simulated in order to compare the solution with experimental data. As a result, detail information of the flow, which was usually difficult to obtain in an experiment, was obtained. On this inlet under the supersonic flow through conditions, the flow was found to be two dimensional in 90% of spanwise direction. In the vicinity of the side-walls, however, three-dimensional separation occurred along the cowl shock. The separation induced a vortex, and the vortex was stretched and swallowed into the throat slot. The ramp bleed ahead of the cowl-shock-impinge line was found to play an important role for avoiding the separation region to spread. A static-wall-pressure comparison between the results and the experimental data showed reasonable agreement. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0289-260X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10097345 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALSP0016040 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL SP-16 |