| タイトル | Perfect bell nozzle parametric and optimization curves |
| 本文（外部サイト） | http://hdl.handle.net/2060/19830016278 |
| 著者（英） | Tuttle, J. L.; Blount, D. H. |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 1983-05-01 |
| 言語 | eng |
| 内容記述 | Nozzle contour data for untruncated Bell nozzles with expansion area ratios to 6100 and a specific heat ratio of 1.2 are provided. Curves for optimization of nozzles for maximum thrust coefficient within a given length, surface area, or area ratio are included. The nozzles are two dimensional axisymmetric and calculations were performed using the method of characteristics. Drag due to wall friction was included in the final thrust coefficient. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 83N24549
NAS 1.61:1104
NASA-RP-1104 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/162634 |
