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机译:基于回归支持向量机的涡轮叶片尖端径向游隙的分布式协同概率设计
School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, PR China;
School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, PR China;
Mechanical dynamic assembly; High pressure turbine; Blade-tip radial running clearance; Probabilistic design; Distributed collaborative response surface method (DCRSM); DCRSM-based support vector machine of regression (SR) (DCSRM);
机译:分布式协同响应面法的HPT叶片尖端径向游隙的概率设计
机译:高压涡轮叶片尖端径向游隙的动态概率设计方法(vol 86,pg 205,2016)
机译:高压透平叶尖径向游隙动态概率设计方法
机译:使用分层响应曲面法的涡轮叶片尖端径向运行清关的鲁棒优化设计
机译:机器学习:线性判别分析,多视图回归和支持向量机的若干进展
机译:新型神经网络回归的基于蠕变的涡轮叶片叶尖间隙可靠性评估
机译:高压汽轮机叶尖径向游隙动态概率设计方法
机译:轴向运行间隙对两台布雷顿循环径向流入涡轮机性能的影响