为了改善离心压气机叶片多工况优化设计时面临的设计空间大、冗余搜索、灵活性不足、优化效率低等问题,提出了基于自由曲面变形技术(free form deform,FFD)的离心压气机复杂曲面叶片参数化方法,建立了叶片局部几何区域与三维空间网格控...为了改善离心压气机叶片多工况优化设计时面临的设计空间大、冗余搜索、灵活性不足、优化效率低等问题,提出了基于自由曲面变形技术(free form deform,FFD)的离心压气机复杂曲面叶片参数化方法,建立了叶片局部几何区域与三维空间网格控制体的映射模型,研究了样条曲线基函数几何特性对叶片几何构型的影响,实现了离心压气机叶片几何外形的局部精细化改型.结合B样条基FFD参数化方法、多目标进化算法和计算流体动力学对复杂叶片的局部区域进行了多工况气动寻优,优化结果表明:在满足约束条件的情况下,流场结构得到进一步的改善,额定工况和常用工况等熵效率分别提高了0.48%和0.40%,喘振裕度分别提升了1.6%和1.8%,利用较少的设计变量实现了离心压气机复杂曲面叶片高效灵活的精细化设计,为离心叶轮的气动优化设计提供了新的理论依据.展开更多
High-fidelity aerodynamic optimization of compressors is afflicted by the"curse of dimensionality",which limits its engineering applications.This paper proposes a new multi-degrees-of-freedom(MDOF)surface pa...High-fidelity aerodynamic optimization of compressors is afflicted by the"curse of dimensionality",which limits its engineering applications.This paper proposes a new multi-degrees-of-freedom(MDOF)surface parameterization method that combines the characteristics of conventional surface parameterization methods,low-dimensionality and surface smoothness,with the advantages of design flexibility and ease of construction.The proposed method is applied to the high-fidelity aerodynamic optimization of Rotor37.An optimized solution is obtained within 111 h by combining a phased optimization strategy based on the idea of modal optimization.To explore a better way of setting the control variables of the blade body,two methods of varying the control points of the suction and pressure surfaces,independent change and synchronous change,are compared.Synchronous change has better flexibility,and under the condition of satisfying the constraints,it increases the efficiency at the design point by 2.2%and the surge margin by 0.5%.This demonstrates the effectiveness of the proposed method in the high-fidelity aerodynamic optimization of compressors.It also provides technical support to solve the"curse of dimensionality"problem.展开更多
文摘为了改善离心压气机叶片多工况优化设计时面临的设计空间大、冗余搜索、灵活性不足、优化效率低等问题,提出了基于自由曲面变形技术(free form deform,FFD)的离心压气机复杂曲面叶片参数化方法,建立了叶片局部几何区域与三维空间网格控制体的映射模型,研究了样条曲线基函数几何特性对叶片几何构型的影响,实现了离心压气机叶片几何外形的局部精细化改型.结合B样条基FFD参数化方法、多目标进化算法和计算流体动力学对复杂叶片的局部区域进行了多工况气动寻优,优化结果表明:在满足约束条件的情况下,流场结构得到进一步的改善,额定工况和常用工况等熵效率分别提高了0.48%和0.40%,喘振裕度分别提升了1.6%和1.8%,利用较少的设计变量实现了离心压气机复杂曲面叶片高效灵活的精细化设计,为离心叶轮的气动优化设计提供了新的理论依据.
基金financially supported by Civil Aircraft Special Project(Grant No.MJZ-2017-D-32(Y81H061A41)).
文摘High-fidelity aerodynamic optimization of compressors is afflicted by the"curse of dimensionality",which limits its engineering applications.This paper proposes a new multi-degrees-of-freedom(MDOF)surface parameterization method that combines the characteristics of conventional surface parameterization methods,low-dimensionality and surface smoothness,with the advantages of design flexibility and ease of construction.The proposed method is applied to the high-fidelity aerodynamic optimization of Rotor37.An optimized solution is obtained within 111 h by combining a phased optimization strategy based on the idea of modal optimization.To explore a better way of setting the control variables of the blade body,two methods of varying the control points of the suction and pressure surfaces,independent change and synchronous change,are compared.Synchronous change has better flexibility,and under the condition of satisfying the constraints,it increases the efficiency at the design point by 2.2%and the surge margin by 0.5%.This demonstrates the effectiveness of the proposed method in the high-fidelity aerodynamic optimization of compressors.It also provides technical support to solve the"curse of dimensionality"problem.
