| dc.contributor | 應數系 | en_US |
| dc.creator (作者) | 謝宗翰 | zh_TW |
| dc.creator (作者) | Shieh,Tzong-Han | en_US |
| dc.creator (作者) | 劉通明 | zh_TW |
| dc.creator (作者) | Liou,Tong-Miin | en_US |
| dc.creator (作者) | 李明融 | zh_TW |
| dc.creator (作者) | Li,Meng-Rong | en_US |
| dc.creator (作者) | Liu,Cheng-Hsin | en_US |
| dc.creator (作者) | Wu,Wen-Jing | en_US |
| dc.date (日期) | 2009.11 | en_US |
| dc.date.accessioned | 7-八月-2014 10:05:18 (UTC+8) | - |
| dc.date.available | 7-八月-2014 10:05:18 (UTC+8) | - |
| dc.date.issued (上傳時間) | 7-八月-2014 10:05:18 (UTC+8) | - |
| dc.identifier.uri (URI) | http://nccur.lib.nccu.edu.tw/handle/140.119/68407 | - |
| dc.description.abstract (摘要) | The flow field for thermal stage separation is carried out and predicted by unsteady numerical simulation with the dynamic moving grids in this work. The overset grids are applied to simulate the relative separating motion of multi-stage rocket. The flow problems and effects of different exhaust holes within the interstage under considering the design of thermal stage separation are systematically computed, discussed and also analyzed. | en_US |
| dc.format.extent | 670335 bytes | - |
| dc.format.mimetype | application/pdf | - |
| dc.language.iso | en_US | - |
| dc.relation (關聯) | International Communications in Heat and Mass Transfer,36(4),342-345 | en_US |
| dc.subject (關鍵詞) | Interstage; Thermal stage separation; Over-expanded nozzle; Overset grids; Navier–Stokes equations | en_US |
| dc.title (題名) | Analysis on numerical results for stage separation with different exhaust holes | en_US |
| dc.type (資料類型) | article | en |
| dc.identifier.doi (DOI) | 10.1016/j.icheatmasstransfer.2009.01.011 | en_US |
| dc.doi.uri (DOI) | http://dx.doi.org/10.1016/j.icheatmasstransfer.2009.01.011 | en_US |
