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基于粒子群算法的可重复使用液体火箭发动机减损优化问题研究 被引量:1
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作者 程玉强 吴建军 刘洪刚 《弹箭与制导学报》 CSCD 北大核心 2009年第2期151-154,共4页
针对可重复使用液体火箭发动机起动过程,研究了系统控制输入序列的变化对以涡轮叶片为代表的关键部件累积损伤的影响。在系统性能变化不大前提下,为使瞬间动态过程中涡轮叶片损伤累积较小,从而提高可重复使用发动机工作寿命和使用次数,... 针对可重复使用液体火箭发动机起动过程,研究了系统控制输入序列的变化对以涡轮叶片为代表的关键部件累积损伤的影响。在系统性能变化不大前提下,为使瞬间动态过程中涡轮叶片损伤累积较小,从而提高可重复使用发动机工作寿命和使用次数,将系统性能函数和涡轮叶片累积损伤量设为目标函数,应用粒子群算法对系统控制输入序列进行优化设计。仿真结果表明:1)在系统性能函数值相同情况下,控制输入序列引起的涡轮叶片累积损伤大不相同;2)选择优化后的控制输入序列能够实现发动机高性能条件下,降低涡轮叶片累积损伤的目的。 展开更多
关键词 可重复使用液体火箭发动机 涡轮叶片 粒子群算法 控制输入序列 性能目标函数
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Enhancement of Performance by Blade Optimization in Two-Stage Ring Blower
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作者 Choon-Man Jang Gi-Young Han 《Journal of Thermal Science》 SCIE EI CAS CSCD 2010年第5期383-389,共7页
This paper describes the shape optimization of an impeller used for two-stage high pressure ring blower.Two shape variables,which are used to define an impeller shape,are introduced to increase the blower performance.... This paper describes the shape optimization of an impeller used for two-stage high pressure ring blower.Two shape variables,which are used to define an impeller shape,are introduced to increase the blower performance.The pressure of a blower is selected as an object function,and the blade optimization is performed by a response surface method.Three-dimensional Navier-Stokes equations are introduced to analyze the internal flow of the blower and to find the value of object function for the training data.Relatively good agreement between experimental measurements and numerical simulation is obtained in the present study.Throughout the shape optimization,it is found that a hub height is effective to increase pressure in the ring blower.The pressure rise for the optimal two-stage ring blower is successfully increased up to 1.86% compared with that of reference at the design flow rate.Local recirculation flow having low velocity is formed in both sides of the impeller outlet by different flow direction of the inlet and outlet of the impeller.Detailed flow field inside the ring blower is also analyzed and discussed. 展开更多
关键词 Ring blower Blower performance Numerical simulation Blade optimization Response surface method
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