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https://ah.lib.nccu.edu.tw/handle/140.119/68407| 題名: | Analysis on numerical results for stage separation with different exhaust holes | 作者: | 謝宗翰 Shieh,Tzong-Han 劉通明 Liou,Tong-Miin 李明融 Li,Meng-Rong Liu,Cheng-Hsin Wu,Wen-Jing |
貢獻者: | 應數系 | 關鍵詞: | Interstage; Thermal stage separation; Over-expanded nozzle; Overset grids; Navier–Stokes equations | 日期: | 2009 | 上傳時間: | 7-Aug-2014 | 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. | 關聯: | International Communications in Heat and Mass Transfer,36(4),342-345 | 資料類型: | article | DOI: | http://dx.doi.org/10.1016/j.icheatmasstransfer.2009.01.011 |
| Appears in Collections: | 期刊論文 |
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| File | Description | Size | Format | |
|---|---|---|---|---|
| 342-345.pdf | 654.62 kB | Adobe PDF2 | View/Open |
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