| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 654198 | International Communications in Heat and Mass Transfer | 2009 | 4 Pages |
Abstract
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.
Keywords
Related Topics
Physical Sciences and Engineering
Chemical Engineering
Fluid Flow and Transfer Processes
Authors
Tzong-Hann Shieh, Tong-Miin Liou, Meng-Rong Li, Cheng-Hsin Liu, Wen-Jing Wu,