The Report of Deflections of Beams and Cantilevers Summary: There are four parts in this big experiment‚ including deflection of a cantilever‚ deflection of a simply supported beam‚ the shape of a deflected beam‚ and circular bending. In these four parts‚ a same set of laboratory instrument and apparatus is used‚ concluding a bracket‚ a moveable digital dial test indicator‚ U-section channel‚ moveable knife-edge‚ and three material beams: brass‚ aluminum‚ and steel. The experiment methods‚ and
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Problem Description: The main purpose of this report is to show how to solve a 3-D finite element model of a cantilever I-shape beam‚ which is subjected to two concentrated loads (P = 1600 lb.) at the flanges of the free end along z axis. In this assignment‚ a convergence study will be used to determine the convergence of the solution with respect to mesh refinement. In addition‚ it will be used to achieve an accurate solution for problems that have sufficiently dense mesh‚ which cannot be solve
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Bending of a Beam Senior Freshman Engineering Laboratories Lab: 2E4A Coordinator: Asst. Prof. Bidisha Ghosh Demonstrator: Concept A transverse load is applied to a beam. The beam changes its shape and experiences bending moment. Internal stresses (bending stress) develop in the beam. In the bent or curved shape‚ the material on the inside of the curve experiences compression and material on the outside of the curve experiences tension. In pure bending‚ the transverse planes in the material
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MM2MS3 Asymmetrical Bending Laboratory Report Date of Laboratory: Name of Student: Student ID: Summary Asymmetrical bending is bending couples acting in a plane of symmetric. If loads do not act in plane of symmetry‚ this leads to deflection in a plane perpendicular to the loading plane as well as in the loading plane. This coupling does not occur if the loading is in principal plane. The experiment was conducted to investigate the deflections of the tip of a cantilever when loaded transversely
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Cantilever Beam Table of Contents Table of Contents 2 1. Introduction 3 2. Theory 3 2.1 Bending Moment and Stresses 3 2.2 Deflection and Slopes 5 3. Equipment 6 4. Procedures 7 4.1 Procedure 1 7 4.2 Procedure 2 8 4.3 Procedure 3 8 5. Results 8 5.1 Results from procedure 1 8 5.2 Results from procedure 2 10 5.3 Results from procedure 3 12 6. Discussion and Error Analysis 14 7. Conclusion 15 1. Introduction During this lab a beam was tested in order to find the relationships
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Laboratory I: Problems 4 and 5 Deflection of an Electron Beam by an Electric Field and Deflection of an Electron Beam and Velocity By: John Greavu Partners: Shane Ruff‚ Hannah Eshenaur‚ & David Sturg Professor: John Capriotti TA: Barun Dhar July 19‚ 2013 OBJECTIVE: The objective of this lab was to scientifically determine the deflection of an electron from its original path due to its passing through an electric field as a function of the electric field strength (problem 4)‚ as well as its initial
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Bending of a Channel Section Experiment Two: Stiffness Report from laboratory work performed on 12 May 2011 as a part of the unit of study CIVL2201 Structural Mechanics Abstract This report has been written to describe an experiment performed on a channel section examining the stiffness of the beam through two differing types of deformation – curvature and deflection. The aim of the experiment was to determine the value of the flexural rigidity (EI) in two different ways; using the curvature
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Abstract: On this project we will try to design an ( I ) construction beam and find lightest weight material that can be used as an construction beam ‚ currently we are taking strength of material course that helping us to learn more about construction beam’s design ‚ we will be going over types of beams ‚ types of loads and beams design ‚ on our own we will research about the materials of beams and try to find the lightest beam’s material that we can use in construction according
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DETERMINATE BEAM AND FRAMEWORK Objective: 1. To Sketch diagram of influence line for reactions‚ shear force and moment for: a. Simply supported beam b. Simply supported beam with one end overhanging c. Simply supported beam with both ends overhanging. 2. To calculate shear force and moment using influence line 3. To determine maximum shear force and moment 4. Calculate Absolute Maximum Moment (MMM) 4.1 INTRODUCTIONS: Influence line is to: Analysis a structure due to moving load along the beam. Show
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Three: Parallam Beam Deflection Lab Group - 1st Mondays‚ Late: Jesse Bertrand‚ Ryan Carmichael‚ Anne Krikorian‚ Noah Marks‚ Ann Murray Report by Ryan Carmichael and Anne Krikorian E6 Laboratory Report – Submitted 12 May 2008 Department of Engineering‚ Swarthmore College Abstract: In this laboratory‚ we determined six different values for the Elastic Flexural Modulus of a 4-by10 (100” x 3.50” x 9.46”) Parallam wood-composite test beam. To accomplish this‚ we loaded the beam at 1/3 span with
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