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

Material type: 文書・図像類

Author: 田寺, 木一ほか

Publisher: 航空宇宙技術研究所

Publication date: 1974-08

Material Format: Digital

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Note (General)：: General three dimensional dynamic equations of motion for a launch vehicle with varying mass are derived, having effects of airframe bending, propella...

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Material Type: 文書・図像類
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
Author/Editor: 田寺, 木一
TATERA, Kiichi
Author Heading: 田寺, 木一
TATERA, Kiichi
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1974-08
Publication Date (W3CDTF): 1974-08
Alternative Title: The Equations of Motion of an Elastic Launch Vehicle with Varying Mass(I)Basic Equations
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-377
No. or year of volume/issue: 377
Volume: 377
Pages: 8-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: jpn
Target Audience: 一般
Note (General): 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.
資料番号: NALTR0377000
レポート番号: NAL TR-377
Access Restrictions: 限定公開
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ