WEKO3
アイテム
{"_buckets": {"deposit": "45e32bc2-b915-4d39-90a4-79c711cabdf5"}, "_deposit": {"created_by": 1, "id": "44625", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "44625"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00044625", "sets": ["1893", "1917"]}, "author_link": ["470398", "470397"], "item_3_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "The Equations of Motion of an Elastic Launch Vehicle with Varying Mass(I)Basic Equations"}]}, "item_3_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "1974-08", "bibliographicIssueDateType": "Issued"}, "bibliographicPageStart": "8", "bibliographicVolumeNumber": "377", "bibliographic_titles": [{"bibliographic_title": "航空宇宙技術研究所報告"}, {"bibliographic_title": "Technical Report of National Aerospace Laboratory TR-377", "bibliographic_titleLang": "en"}]}]}, "item_3_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "General three dimensional dynamic equations of motion for a launch vehicle with varying mass are derived, having effects of airframe bending, propellant sloshing, propellant flow and engine swivelling into account. In this paper, the effect of propellant flow are concidered as reaction forces of propellant to airframe, and using the theory of continuum mechanics the time rate of change of integrals of some quantities are being transfered out of the system. Sloshing and bending equations are derived accuratly,in view of practical analysis of the whole motion of the vehicle.", "subitem_description_type": "Other"}]}, "item_3_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: NALTR0377000", "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-377", "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機体第一部"}]}, "item_3_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "First Airframe Division, National Aerospace Laboratory(NAL)"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "田寺, 木一"}], "nameIdentifiers": [{"nameIdentifier": "470397", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "TATERA, Kiichi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "470398", "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": "naltr00377.pdf", "filesize": [{"value": "749.9 kB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 749900.0, "url": {"label": "naltr00377.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/44625/files/naltr00377.pdf"}, "version_id": "3474bb76-5eac-4b84-b6fd-78761afb8018"}]}, "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": "質量が変化する弾性飛しょう体の運動方程式(Ⅰ)基礎方程式", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "質量が変化する弾性飛しょう体の運動方程式(Ⅰ)基礎方程式"}]}, "item_type_id": "3", "owner": "1", "path": ["1893", "1917"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/44625", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "44625", "relation": {}, "relation_version_is_last": true, "title": ["質量が変化する弾性飛しょう体の運動方程式(Ⅰ)基礎方程式"], "weko_shared_id": -1}
質量が変化する弾性飛しょう体の運動方程式(Ⅰ)基礎方程式
https://jaxa.repo.nii.ac.jp/records/44625
https://jaxa.repo.nii.ac.jp/records/446251eaf8f27-1e82-46fc-9dd3-61ea8bab9d3f
名前 / ファイル | ライセンス | アクション |
---|---|---|
naltr00377.pdf (749.9 kB)
|
|
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 | 質量が変化する弾性飛しょう体の運動方程式(Ⅰ)基礎方程式 | |||||
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 | The Equations of Motion of an Elastic Launch Vehicle with Varying Mass(I)Basic Equations | |||||
著者 |
田寺, 木一
× 田寺, 木一× TATERA, Kiichi |
|||||
著者所属 | ||||||
航空宇宙技術研究所機体第一部 | ||||||
著者所属(英) | ||||||
en | ||||||
First Airframe Division, National Aerospace Laboratory(NAL) | ||||||
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報告 en : Technical Report of National Aerospace Laboratory TR-377 巻 377, p. 8, 発行日 1974-08 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | General three dimensional dynamic equations of motion for a launch vehicle with varying mass are derived, having effects of airframe bending, propellant sloshing, propellant flow and engine swivelling into account. In this paper, the effect of propellant flow are concidered as reaction forces of propellant to airframe, and using the theory of continuum mechanics the time rate of change of integrals of some quantities are being transfered out of the system. Sloshing and bending equations are derived accuratly,in view of practical analysis of the whole motion of the vehicle. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTR0377000 | |||||
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 TR-377 |