Question

Matlab problem!Description The deflection of a cantilevered beam with a point load is Wx2 :), 0<xsa Wa? ATT (3x-a), a SXSL where E= Youngs

0 0
Add a comment Improve this question Transcribed image text
Answer #1

`Hey,

Note: Brother if you have any queries related the answer please do comment. I would be very happy to resolve all your queries.

clc
clear all
close all
E=30*10^6;
I=0.163;
L=10;
W=1000;
a=3;
figure;
BeamCantPoint(E,I,L,a,W);
title('For a=3');
a=0:2:10;
figure;
BeamCantPoint(E,I,L,a,W);
title('For a=0 to 10')


function BeamCantPoint(E,I,L,a,W)
hold on;
for j=1:length(a)
x=0:0.01:L;
y=[];
for i=1:length(x)
if(x(i)<=a(j))
y(i)=-W*x(i)^2/(6*E*I)*(3*a(j)-x(i));
else
y(i)=-W*x(i)^2/(6*E*I)*(3*x(i)-a(j));
end
end
plot(x,y);
end
end

- 5 x Pradeep APPS EDITOR PUBLISH VIEW BA A ? - Search Documentation - OX MATLAB R2018a HOME PLOTS Figure 1 New Eile Edit Vie

Kindly revert for any queries

Thanks.

Add a comment
Know the answer?
Add Answer to:
Matlab problem! Description The deflection of a cantilevered beam with a point load is Wx2 :),...
Your Answer:

Post as a guest

Your Name:

What's your source?

Earn Coins

Coins can be redeemed for fabulous gifts.

Not the answer you're looking for? Ask your own homework help question. Our experts will answer your question WITHIN MINUTES for Free.
Similar Homework Help Questions
  • Problem statement Beam Deflection: Given the elastic deflection equation for a beam with the boundary and...

    Problem statement Beam Deflection: Given the elastic deflection equation for a beam with the boundary and loading conditions shown below, determine the maximum downward deflection (i.e. where dy/dx = 0) of a beam under the linearly increasing load wo = 10 kN/m. Use the following parameter values: L = 10m, E = 5x108 kN/m², 1 = 3x10-4 m4. Use the initial bracket guesses of XL = 0 m and xu = 10 m. Wo. wol(x5 + 2L?x3 – L^x), (1)...

  • 2. The governing differential equation that relates the deflection y of a beam to the load w ia w...

    2. The governing differential equation that relates the deflection y of a beam to the load w ia where both y and w are are functions of r. In the above equation, E is the modulus of elasticity and I is the moment of inertia of the beam. For the beam and loading shown in the figure, first de m, E = 200 GPa, 1 = 100 × 106 mm4 and uo 100 kN/m and determine the maximum deflection. Note...

  • Uniform beam under distributed load

    Case 1: Uniform beam under distributed load.In the shown Figure, a uniform beam subject to a linearly increasing distributed load. The deflection \(y(\mathrm{~m})\) can be expressed by \(y=\frac{w_{o}}{120 E I L}\left(-x^{5}+2 L^{2} x^{3}-L^{4} x\right)\)Where \(E\) is the modulus of elasticity and \(I\) is the moment of inertia \(\left(\mathrm{m}^{4}\right), L\) length of beam.Use the following parameters \(L=600 \mathrm{~cm}\), \(E=50,000 \mathrm{kN} / \mathrm{cm}^{2}, I=30.000 \mathrm{~cm}^{4}, w_{\mathrm{o}}=2.5\)\(\mathrm{kN} / \mathrm{cm}\), to find the requirements1) Develop MATLAB code to determine the point of maximum deflection...

  • Problem 1.1 Consider the beam bending problem below 2 Po Consider the beam to be homogenous...

    Problem 1.1 Consider the beam bending problem below 2 Po Consider the beam to be homogenous and linearly elastic, with length L, stiffness E, and moment of inertia I. The beam is cantilevered at x = 0 an d is supported by a linear spring of stiffness k at x-L. A uniformly distributed transverse load po (N/m) is applied to the upper surface a) Write and solve the GDE to obtain the exact solution for the deflection w(x) of this...

  • EMT 101- Engineering Programming Homework 3 Deflection of an I-Beam(100 %) You are to develop a program that calculates and plots the vertical deflection of a beam subjected to a force acting on it...

    EMT 101- Engineering Programming Homework 3 Deflection of an I-Beam(100 %) You are to develop a program that calculates and plots the vertical deflection of a beam subjected to a force acting on it as given in Figure 1. The I-Beam has length, L 2m with its left end fixed at the wall (no deflection at wall) The right end of the beam is applied with a vertical load force P with a vertical deflection function (3L -a) EI wherer...

  • SOLVE USING MATLAB PLEASE THANKS! The governing differential equation for the deflection of a cantilever beam...

    SOLVE USING MATLAB PLEASE THANKS! The governing differential equation for the deflection of a cantilever beam subjected to a point load at its free end (Fig. 1) is given by: 2 dx2 where E is elastic modulus, Izz is beam moment of inertia, y 1s beam deflection, P is the point load, and x is the distance along the beam measured from the free end. The boundary conditions are the deflection y(L) is zero and the slope (dy/dx) at x-L...

  • (a) A cantilever beam shown in Figure 6 is subjected to a concentrated load P. Deflection...

    (a) A cantilever beam shown in Figure 6 is subjected to a concentrated load P. Deflection of the beam at each point can be defined by the following equations: 6EI Pa 6EI F3x-a) for axx<l The following MATLAB code calculates and plots the deflection diagram for a beam with 1-4 m, d1 = 3 m, b = 1 m,E>210 x 10, Pa, 1 = 285 x 10-6 m4 and P = 20 kN. Find at least FOUR errors in the...

  • please please help! Statically Indeterminate Propped Cantilevered Beam Reaction and Deflection Derivation 1. Determine the reactions...

    please please help! Statically Indeterminate Propped Cantilevered Beam Reaction and Deflection Derivation 1. Determine the reactions R4, Rg, and M, and the elastic equation for the section of the beam between the wall and the load P. 2. Note: It will take 3 solutions to solve for the elastic equations for the entire beam: 0<x<d, d<x<s, and s SXSL 1. The derivation of the elastic equation for the section between the wall and the load (0 <x<d) is derived above....

  • The deflection y, in a simple supported beam with a uniform load q and a tensile load T is given by dx2 El 2EI Wher...

    The deflection y, in a simple supported beam with a uniform load q and a tensile load T is given by dx2 El 2EI Where x location along the beam, in meter T-Applied Tension E-Young's Modulus of elasticity of the beam 1= Second moment of inertia of the beam Applied uniform loading (N/m), L- length of the beam in meter Given that T-32 kN, q = 945.7 kN/m, L = 2.0 meter, E = 206 GPa and 1 4.99 x...

  • In Appendix C, see the simply supported beam with a uniformly distributed load. Be careful with...

    In Appendix C, see the simply supported beam with a uniformly distributed load. Be careful with units and the sign convention. For this calculation, the overhung part of the beam from C to D can be ignored, and the beam is treated as a simply supported beam of length 2L1. Be careful with units and the sign convention. The simply supported beam consists of a W530 × 66 structural steel wide-flange shape [ E = 200 GPa; I = 351...

ADVERTISEMENT
Free Homework Help App
Download From Google Play
Scan Your Homework
to Get Instant Free Answers
Need Online Homework Help?
Ask a Question
Get Answers For Free
Most questions answered within 3 hours.
ADVERTISEMENT
ADVERTISEMENT