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低展弦比CAES向心涡轮叶顶型线的正交设计优化(英文) 被引量:1
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作者 王星 李文 +3 位作者 张雪辉 朱阳历 左志涛 陈海生 《风机技术》 2019年第1期11-21,I0008,共12页
为降低叶顶泄漏损失,本文首次将NACA翼型引入向心涡轮,并采用正交试验设计和计算流体动力学(CFD)方法获得了具有最优NACA叶顶型线的向心涡轮叶片,并揭示了该叶片对叶顶泄漏损失的控制机理。结果表明,最优NACA叶顶型线具有较大的前缘内... 为降低叶顶泄漏损失,本文首次将NACA翼型引入向心涡轮,并采用正交试验设计和计算流体动力学(CFD)方法获得了具有最优NACA叶顶型线的向心涡轮叶片,并揭示了该叶片对叶顶泄漏损失的控制机理。结果表明,最优NACA叶顶型线具有较大的前缘内接圆半径、较小的尾缘厚度,以及更靠近前缘的最大厚度位置。其内接圆半径和最大厚度位置对向心涡轮等熵效率的影响度也随叶顶间隙增加而增大。当叶顶间隙为8%出口叶高时,最优NACA叶顶型线可使向心涡轮等熵效率提高1.47%,并使向心涡轮能够在非设计工况下具有较高效率。该型线能够降低尾缘附近的叶顶泄漏速度,减弱泄漏流与主流掺混强度,使流动损失降低。 展开更多
关键词 Radial EXPANDER Optimization BLADE Tip Profile CAES Orthogonal Experiment Design
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Fatigue-creep interaction based on continuum damage mechanics for AISI H13 hot work tool steel at elevated temperatures 被引量:7
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作者 hai-sheng chen Yong-qin Wang +2 位作者 Wei-qi Du Liang Wu Yuan-xin LUO 《Journal of Iron and Steel Research(International)》 SCIE EI CAS CSCD 2018年第5期580-588,共9页
AISI H13 (4Cr5MoSiV1) is one of the commonly used materials for extrusion tool, and it suffers from fatigue-creep damage during the hot extrusion process. Stress-controlled fatigue and creep-fatigue interaction test... AISI H13 (4Cr5MoSiV1) is one of the commonly used materials for extrusion tool, and it suffers from fatigue-creep damage during the hot extrusion process. Stress-controlled fatigue and creep-fatigue interaction tests were carried out at 500℃ to investigate its damage evolution. The accumulated plastic strain was selected to define the damage variable due to its clear physical meaning. A new fatigue-creep interaction damage model was proposed on the basis of continuum damage mechanics. A new equivalent impulse density for fatigue-creep tests was proposed to incorporate the holding time effect by transforming creep impulse density into fatigue impulse density. The experimental results indicated that the damage model is able to describe the damage evolution under these working conditions. 展开更多
关键词 AISI H13 hot work tool steel · Fatigue-creep · Damage evolution ·Continuum damage mechanics ·Nonlinear interaction · Damage exponent
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