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Deflection (engineering)

About: Deflection (engineering) is a research topic. Over the lifetime, 30862 publications have been published within this topic receiving 298849 citations.


Papers
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Journal ArticleDOI
TL;DR: In this paper, a theoretical and experimental study of the response of a damaged Euler-Bernoulli beam traversed by a moving mass is presented, where damage is modelled through rotational springs whose compliance is evaluated using linear elastic fracture mechanics.

91 citations

Journal ArticleDOI
TL;DR: In this article, a loaded tooth contact analysis (LTCA) program is presented to predict the motion error of spiral bevel gear sets under load, and explores some of the influences of the unloaded motion error curve shape and amplitude over the kinematical behavior under load.

91 citations

Journal ArticleDOI
TL;DR: In this paper, a numerical method is developed for solving the governing nonlinear differential equations of this problem, and two types of loading conditions are included-an impulsive load and an instantaneous ly applied step load with infinite duration.
Abstract: The behavior of axisymmetric dynamic snap-through of elastic, clamped shallow spherical shells under a uniform pressure has been investigated by.several authors. In most of the previous work, approximate methods were used, and as yet no positive conclusion has been made on the critical load for snap-through. In this paper, a numerical method is developed for solving the governing nonlinear differential equations of this problem. Two types of loading conditions are included-—an impulsive load and an instantaneous ly applied step load with infinite duration. In the case of impulsive loading, it is found from the quasi-static problem under zero load that the only equilibrium, position of the shell is its undeformed configuration. Hence, if we define the dynamic snap-through based on the finite jump behavior of deflection then there is no possibility for dynamic snap-through under impulsive loading. In the case of step loading, the snap-through loads are evaluated for a wide range of the geometrical parameter of the shell. Comparison of the present calculated critical loads with the previous results from approximate methods is made. It is found that the present critical load checks closely with an experimental value of the critical load for one value of the geometrical parameter of the shell.

91 citations

01 May 1946
TL;DR: In this paper, a general solution for the determination of loads carried by individual bolts in symmetrical butt joints is presented, where test specimens made of 24S-T aluminum-alloy plates fastened by two or three 1/4-inch alloy-steel bolts with the bolts in a single line in line with the applied load.
Abstract: Report presenting a general solution for the determination of loads carried by individual bolts in symmetrical butt joints. Testing was conducted on test specimens made of 24S-T aluminum-alloy plates fastened by two or three 1/4-inch alloy-steel bolts with the bolts in a single line in line with the applied load. Results regarding the determination of bolt loads and deflections from test data, curves of joint load against bolt load, and curves of bolt load against deflection are provided.

90 citations

Journal ArticleDOI
TL;DR: In this article, the authors investigated the strength and ductility aspects of reinforced concrete (RC) beams strengthened with an externally bonded carbon fiber reinforced polymer (CFRP) laminate and examined how such retrofitting affects strength, deflection, curvature and energy, as exemplified by the area under the load-deflection curve of the strengthened composite beam.
Abstract: The objective of this study is to investigate the strength and ductility aspects of reinforced concrete (RC) beams strengthened with an externally bonded carbon fiber reinforced polymer (CFRP) laminate and to examine how such retrofitting affects strength, deflection, curvature, and energy, as exemplified by the area under the load-deflection curve of the strengthened composite beam. Three series of tests on eleven RC beams were carried out and their ultimate load capacities and ductilities evaluated. The variables in the experimental program were longitudinal steel ratio, volume of internal stirrups, and the location and configuration of external anchorages. The results show that both deflection and energy absorption are drastically reduced when beams are strengthened with bonded CFRP plates without external anchorages. Suitably designed and positioned external anchorages allow much of this lost ductility to be regained; however, even then the ductility of the strengthened beam cannot be restored to its original level. It is shown that definitions of ductility based on deflection and energy are able to give a good and rational representation of the physical aspects of ductility of RC beams strengthened with bonded CFRP laminates with or without external anchorages. The results show that the effects on ductility arising from strengthening existing RC beams with CFRP laminates cannot be ignored, even if it is not clear at this stage how to apply the concept of ductility indices and ductility ratios developed in this paper in design practice.

90 citations


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Performance
Metrics
No. of papers in the topic in previous years
YearPapers
202247
20211,006
20201,140
20191,262
20181,195
20171,215