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    政大機構典藏 > 理學院 > 應用數學系 > 期刊論文 >  Item 140.119/68407
    Please use this identifier to cite or link to this item: https://nccur.lib.nccu.edu.tw/handle/140.119/68407

    Title: Analysis on numerical results for stage separation with different exhaust holes
    Authors: 謝宗翰
    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
    DOI: 10.1016/j.icheatmasstransfer.2009.01.011
    Appears in Collections:[應用數學系] 期刊論文

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