Please use this identifier to cite or link to this item: https://ah.nccu.edu.tw/handle/140.119/68407


Title: Analysis on numerical results for stage separation with different exhaust holes
Authors: 謝宗翰
Shieh,Tzong-Han
劉通明
Liou,Tong-Miin
李明融
Li,Meng-Rong
Liu,Cheng-Hsin
Wu,Wen-Jing
Contributors: 應數系
Keywords: Interstage;Thermal stage separation;Over-expanded nozzle;Overset grids;Navier–Stokes equations
Date: 2009.11
Issue Date: 2014-08-07 10:05:18 (UTC+8)
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.
Relation: International Communications in Heat and Mass Transfer,36(4),342-345
Data Type: article
DOI 連結: http://dx.doi.org/10.1016/j.icheatmasstransfer.2009.01.011
Appears in Collections:[應用數學系] 期刊論文

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