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机译:基于DCERSM的多分量多物理场涡轮叶片尖端径向间隙瞬态概率分析
Hong Kong Polytech Univ, Dept Mech Engn, Hong Kong, Hong Kong, Peoples R China|Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China;
Hong Kong Polytech Univ, Dept Mech Engn, Hong Kong, Hong Kong, Peoples R China;
Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China;
Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China;
Beihang Univ, Sch Comp Engn & Sci, Beijing 100191, Peoples R China;
High pressure turbine; Blade-tip radial running clearance; Dynamic probabilistic analysis; Distributed collaborative extremum response surface method; Multi-object multi-disciplinary;
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)
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机译:航空发动机高压汽轮机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:ATEC:《气动涡轮发动机规范》,用于分析瞬态和动态燃气涡轮发动机系统的运行
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:基于DCERSM的多分量多物理场涡轮叶片径向间隙瞬态概率分析
机译:涡轮叶片尖端间隙激励力