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表面效应对热-机多孔悬臂纳米梁力学性能的影响

李清禄 赵煊贺 张靖华 潘兆一

航空材料学报2024,Vol.44Issue(3):124-131,8.
航空材料学报2024,Vol.44Issue(3):124-131,8.DOI:10.11868/j.issn.1005-5053.2022.000176

表面效应对热-机多孔悬臂纳米梁力学性能的影响

Influence of surface effect on mechanical properties of thermo-mechanical porous cantilever nanobeams

李清禄 1赵煊贺 1张靖华 1潘兆一2

作者信息

  • 1. 兰州理工大学理学院,兰州 730050
  • 2. 甘肃新农生态能源环保科技有限公司,甘肃定西 730500
  • 折叠

摘要

Abstract

The surface effect has an important influence on the mechanical properties of nanostructures.Many micro and nano-scale structures on aircraft can be simplified as cantilever beams.In this paper,the influence of surface effect on the nonlinear mechanical response of gradient porous material nano cantilever under follower load at high temperature was analyzed.Based on Gurtin-Murdoch's surface elastic theory and nonlinear beam theory,the nonlinear governing differential equations of gradient porous material beam under follower load and temperature field were established.It was assumed that the properties of gradient porous materials change continuously in the entire thickness range,and there were two kinds of non-uniform porosity distribution patterns in cosine form along the thickness.The nonlinear mechanical response of the gradient porous material cantilever nanobeam under thermal follower load was solved by shooting method.The numerical solutions of the nonlinear mechanical response of the cantilever under various porosity coefficients and different non-uniform temperature rises were obtained.The effects of the material surface elastic constants and surface stresses on the mechanical response of the cantilever were discussed in detail.The results show that the mechanical behaviors of beams are different under different porosity coefficients and different non-uniform temperature rises.The nanobeams exhibit very significant surface effects.

关键词

梯度多孔材料/悬臂梁/随从载荷/表面残余应力/表面效应

Key words

graded porous materials/cantilever beam/follower force/surface residual stress/surface effect

分类

航空航天

引用本文复制引用

李清禄,赵煊贺,张靖华,潘兆一..表面效应对热-机多孔悬臂纳米梁力学性能的影响[J].航空材料学报,2024,44(3):124-131,8.

基金项目

国家自然科学基金项目(12062010,12362009) (12062010,12362009)

甘肃省自然科学基金重点项目(23JRRA775) (23JRRA775)

航空材料学报

OA北大核心CSTPCD

1005-5053

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