| タイトル | Suspension-line wave motion during the lines-first parachute unfurling process |
| 著者（英） | Poole, L. R.; Whitesides, J. L. |
| 発行日 | 1974-01-01 |
| 言語 | eng |
| 内容記述 | A new mathematical approach to modeling the lines-first parachute unfurling process is presented. The unfurling process is treated as two distinct phases: a suspension-line unfurling phase, during which a massless-spring model of the suspension-line elasticity may be employed; and a canopy unfurling phase, during which a formulation considering suspension-line wave mechanics is employed. Histories of unfurled length and tension at the vehicle obtained using the model are compared with flight test data, and generally good agreement is observed. |
| NASA分類 | AIRCRAFT |
| レポートNO | 74A17013 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/454315 |
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