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On the Dynamic Stability of Rockets
https://jaxa.repo.nii.ac.jp/records/34632
https://jaxa.repo.nii.ac.jp/records/3463294d62bf1-8635-4c22-83ce-c9b934e9f827
名前 / ファイル | ライセンス | アクション |
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SA2404929.pdf (1.7 MB)
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Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | On the Dynamic Stability of Rockets | |||||
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 |
TOMITA, Bunji
× TOMITA, Bunji |
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出版者 | ||||||
出版者 | 東京大学航空研究所 | |||||
出版者(英) | ||||||
出版者 | Aeronautical Research Institute, University of Tokyo | |||||
書誌情報 |
東京大學航空研究所報告 en : Report/Aeronautical Research Institute, University of Tokyo 巻 29, 号 7, p. 85-118, 発行日 1964-03 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The general equations of motion are derived for spinning elastic rocket with respect to axes attached to the rocket. The equations contain a force and moment system that includes, in addition to the usual quasisteady forces and moments, those due to Magnus effects. As a result, the stability criteria for spinning elastic rocket are approximately derived, including as special cases, those such as for the case of rigid body and for the case of nonspinning elastic rocket, which have been analyzed. Comparing these analytical results with the digital computational results, the applicability of these stability criteria is examined and from these results, empirical formulas for stability boundaries are also presented. Furthermore, clasifying the stability boundaries into seviral types according to the characteristics of motion of rocket at the critical speed, and the physical meaning of each stability boundary is also explained. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0376-1061 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA00514444 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: SA2404929000 |