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THE THERMAL-ELASTIC THREE-DIMENSION FINITE ELEMENT STRESS ANALYSIS OF HIGH-PRESSURE TURBINE-BLADE

机译：高压涡轮叶片的热弹性三维有限元应力分析

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The thermal-elastic stress analysis of high-pressure turbine-lade is studied in this paper, especially about the calculating method of stress at blade root and tenon tooth, and the distributing of thermal-elastic stresses on the whole blade is thus obtained with the method presented.

机译：本文研究了高压涡轮叶片的热弹性应力分析，特别是叶片根部和榫齿处的应力计算方法，从而得到了整个叶片的热弹性应力分布。方法介绍。

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《Machine elements》|1996年|P.133|共1页
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Meng Chunling; Rao Shouqi;
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中图分类机械零件及传动装置;
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4. THE THERMAL-ELASTIC THREE-DIMENSION FINITE ELEMENT STRESS ANALYSIS OF HIGH-PRESSURE TURBINE-BLADE [C] . Meng Chunling, Rao Shouqi Machine elements . 1996

机译：高压涡轮叶片的热弹性三维有限元应力分析
5. Coupling axisymmetric and plane stress/axial finite elements for the stress analysis of an aircraft engine compressor. [D] . Immaneni, Dinesh. 2007

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6. A three-dimension finite element analysis to evaluate the stress distribution in tooth supported 5-unit intermediate abutment prosthesis with rigid and nonrigid connector [O] . Ritesh Modi, Shivani Kohli, K. Rajeshwari, 2015

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7. A three-dimension finite element analysis to evaluate the stress distribution in tooth supported 5-unit intermediate abutment prosthesis with rigid and nonrigid connector [O] . Ritesh Modi, Shivani Kohli, K. Rajeshwari, 2015

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8. Special Hybrid Stress Finite Elements for the Analysis of Interface StressDistribution in Adhesive Joints [R] . Saether, E., Weight, K. 1994

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THE THERMAL-ELASTIC THREE-DIMENSION FINITE ELEMENT STRESS ANALYSIS OF HIGH-PRESSURE TURBINE-BLADE

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