| タイトル | Numerical solution of equations governing longitudinal suspension line wave motion during the parachute unfurling process |
| 本文（外部サイト） | http://hdl.handle.net/2060/19730020256 |
| 著者（英） | Poole, L. R. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1973-05-01 |
| 言語 | eng |
| 内容記述 | Equations are presented which govern the dynamics of the lines-first parachute unfurling process, including wave motion in the parachute suspension lines. Techniques are developed for obtaining numerical solutions to the governing equations. Histories of tension at test data, and generally good agreement is observed. Errors in computed results are attributed to several areas of uncertainty, the most significant being a poorly defined boundary condition on the wave motion at the vehicle-suspension line boundary. |
| NASA分類 | AIRCRAFT |
| レポートNO | 73N28988
NASA-TM-X-69498 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/198279 |
