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On the Dynamic Behavior of Balloon during its Launch; Application of Panel Method and Extension to Unsteady Problem
https://jaxa.repo.nii.ac.jp/records/31387
https://jaxa.repo.nii.ac.jp/records/313871778a2a6-3119-40d2-b7b5-8e0cfb140c1b
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
SA0035020.pdf (1.1 MB)
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| Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|
| 公開日 | 2015-03-26 | |||||||||
| タイトル | ||||||||||
| タイトル | On the Dynamic Behavior of Balloon during its Launch; Application of Panel Method and Extension to Unsteady Problem | |||||||||
| 言語 | en | |||||||||
| 言語 | ||||||||||
| 言語 | eng | |||||||||
| キーワード | ||||||||||
| 言語 | en | |||||||||
| 主題Scheme | Other | |||||||||
| 主題 | Panel method, Unsteady flow, Balloon, Numerical simulation | |||||||||
| 資源タイプ | ||||||||||
| 資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||||||
| 資源タイプ | departmental bulletin paper | |||||||||
| 著者 |
稲谷, 芳文
× 稲谷, 芳文
× INATANI, Yoshifumi
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| 出版者 | ||||||||||
| 出版者 | 宇宙科学研究所 | |||||||||
| 出版者（英） | ||||||||||
| 出版者 | Institute of Space and Astronautical Science | |||||||||
| 書誌情報 |
en : The Institute of Space and Astronautical Science report 巻 622, p. 1-22, 発行日 1987-07 |
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| 抄録（英） | ||||||||||
| 内容記述タイプ | Other | |||||||||
| 内容記述 | Boundary integral method (Panel method) has been applied and extended to investigate the unsteady problem in which body shape is deformed dynamically due to flow effects inside or outside the body. Such an unsteady effect has been represented by use of extension of conventional panel method. The interaction between the deformation of body and the flow field is represented as "Virtual Mass Matrix", and the motion of the body surface and the flow field are solved by tracing the control points distributed on the body surface. Inegral relations of the singularity distributed on the panel are also presented. Techniques developed in this study are applied to the dynamic simulation of balloon launching. A series of simulation study has been carried out and the deformation of a balloon during its launch has been followed. The result of the simulation realizes a dynamic behavior of balloon launching and load history of ballon membrane is obtained. | |||||||||
| ISSN | ||||||||||
| 収録物識別子タイプ | ISSN | |||||||||
| 収録物識別子 | 0285-6808 | |||||||||
| 書誌レコードID | ||||||||||
| 収録物識別子タイプ | NCID | |||||||||
| 収録物識別子 | AA10632072 | |||||||||
| 資料番号 | ||||||||||
| 内容記述タイプ | Other | |||||||||
| 内容記述 | 資料番号: SA0035020000 | |||||||||
