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A Self-consistent Tension Shell Structure for Application to Aerobraking Vehicle and its Aerodynamic Characteristics
https://jaxa.repo.nii.ac.jp/records/31331
https://jaxa.repo.nii.ac.jp/records/313317683b323-430e-4fab-a626-7fa08ee542d7
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
SA0033604.pdf (672.3 kB)
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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 | A Self-consistent Tension Shell Structure for Application to Aerobraking Vehicle and its Aerodynamic Characteristics | |||||||
| 言語 | en | |||||||
| 言語 | ||||||||
| 言語 | eng | |||||||
| 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 |
ABE, Takashi
× ABE, Takashi
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| 著者所属（英） | ||||||||
| en | ||||||||
| The Institute of Space and Astronautical Science. | ||||||||
| 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. S.P. : An Aerodynamics in Relation to an Aeroassisted Orbit Transfer Vehicle 巻 7, p. 3-14, 発行日 1988-11 |
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| 抄録（英） | ||||||||
| 内容記述タイプ | Other | |||||||
| 内容記述 | A new method determining a tension shell structure for an application to an aerobraking vehicle is proposed. In this method, the tension shell configuration can be determined self-consistently in that the pressure distribution which is used to determine the shell configuration can be consistent with the one appearing on the configuration. The aerodynamic characteristics of the tension shell is also investigated numerically. | |||||||
| ISSN | ||||||||
| 収録物識別子タイプ | ISSN | |||||||
| 収録物識別子 | 0288-433X | |||||||
| 書誌レコードID | ||||||||
| 収録物識別子タイプ | NCID | |||||||
| 収録物識別子 | AA10455137 | |||||||
| 資料番号 | ||||||||
| 内容記述タイプ | Other | |||||||
| 内容記述 | 資料番号: SA0033604000 | |||||||
