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用能量法计算涡轮盘偏心孔边局部应力
引用本文:吕文林,魏邦旭.用能量法计算涡轮盘偏心孔边局部应力[J].航空动力学报,1989,4(2):179-182,198.
作者姓名:吕文林  魏邦旭
作者单位:西北工业大学 (吕文林),西北工业大学(魏邦旭)
摘    要:为在弹塑性状态下计算孔边局部应力,本文基于能量法则,推导出计算孔边局部应力的方法。本文的方法简单实用,准确度较修正诺伯法计算结果要高,文中附有涡轮盘偏心孔的计算实例,并对计算结果进行了分析。

收稿时间:6/1/1988 12:00:00 AM

AN ENERGY METHOD FOR CALCULATING THE LOCAL STRESS AT AN ECCENTRIC HOLE IN A TURBINE DISK
Lu Wenlin and Wei Bangxu.AN ENERGY METHOD FOR CALCULATING THE LOCAL STRESS AT AN ECCENTRIC HOLE IN A TURBINE DISK[J].Journal of Aerospace Power,1989,4(2):179-182,198.
Authors:Lu Wenlin and Wei Bangxu
Institution:Northwestern Polytechnical University;Northwestern Polytechnical University
Abstract:A new method based on energy principle is derived to calculate local stress at an eccentric hole in a turbine disk under the elasto-plastic conditions. This method is not only simpleand practical, but also able to obtain more accurate results than those calculated by the modified Neu-ber method. A numerical example is also presented in this paper.
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