Large deflections of a spring-hinged tapered cantilever beam with a rotational distributed loading

IF 1.4 4区工程技术 Q2 ENGINEERING, AEROSPACE Aeronautical Journal Pub Date : 1987-11-01 DOI:10.1017/S0001924000021667

B. Nageswara Rao, G. Venkateswara Rao

引用次数: 4

Abstract

Summary Large deflection problem of a spring loaded hinged nonuniform cantilever beam subjected to a rotational distributed loading is formulated by means of a second-order non-linear integro-differential equation. The problem is examined by considering the beam of rectangular cross-section with linear depth taper subjected to a uniform rotational distributed load. The elastic curves of a beam for this special case are presented.

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具有旋转分布载荷的弹簧铰接锥形悬臂梁的大挠度

用二阶非线性积分-微分方程表达了受旋转分布载荷作用的弹簧加载铰接非均匀悬臂梁的大挠度问题。通过考虑受均匀旋转分布荷载作用的具有线性深度锥度的矩形截面梁来检验这一问题。给出了这种特殊情况下梁的弹性曲线。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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来源期刊

Aeronautical Journal 工程技术-工程：宇航

CiteScore

3.70

自引率

14.30%

发文量

审稿时长

6-12 weeks

期刊介绍： The Aeronautical Journal contains original papers on all aspects of research, design and development, construction and operation of aircraft and space vehicles. Papers are therefore solicited on all aspects of research, design and development, construction and operation of aircraft and space vehicles. Papers are also welcomed which review, comprehensively, the results of recent research developments in any of the above topics.

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