Numerical computation of solid rocket motor insulation layer temperature by finite element method

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作者：
School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China [1 ]
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来源：
Hangkong Dongli Xuebao | 2009年 / 6卷 / 1407-1412期
关键词：
Boundary conditions - Heat convection - Numerical methods - Rockets - Rocket engines - Insulation - Heat flux - Pyrolysis;
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