I assumed you asked to write a MATLAB programme. So here is the matlab programme for the given question
%==================Here is the matlab code==================
clear all
close all
clc
P=3e3; %in N
E=7e10; % in N/m^2
h=100e-3; % in m
b=5e-3; % in m
t=8e-3; % in m
L=2; %in m
x=0:0.1:L;
for i=1:length(x)
l=x(i);
% calculating the I(x) using the subroutine
Ix=MI(h,b,t,l,L);
% calculating the deflection
vx=(P*x.^2.*(3*L-x))/(E*Ix);
end
% plotting the deflection
plot(x,vx)
xlabel('length in m')
ylabel('deflection in m')
%=============== a subroutine to calculate the moment of inertia==================
function Ix=MI(h,b,t,l,L)
if (l>=0&&l<L/2)
w=150e-3;
else
w=90e-3;
end
Ix=(w*h^3-(h-2*t)^3*(w-b))/12;
end
%===============End of the matlab code=============================
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...
2. a. An edge beam with sectional dimensions is shown in Fig.3. i. Determine the location of its centriod from point 0. ii. Determine its moment of inertia in x-x direction about centriod. A y 150mm 40mm 35mm 300mm V --> X Fig. 3 2. b. Determine the mid-span deflection of a 3m long simply supported R.C. beam which is subject to a gravity UDL of 10 kN/m with a cross section as shown in Fig. 3 (E = 35kN/mm²).
4. (25 pt.) The beam subjected to a uniform distributed load as shown in Figure 4(a) has a triangular cross-section as shown in Figure 4(b). 1) (6 pt.) Determine mathematical descriptions of the shear force function V(x) and the moment function M(x). 2) (6 pt.) Draw the shear and moment diagrams for the beam. 3) (5 pt.) What is the maximum internal moment Mmar in the beam? Where on the beam does it occur? 4) (8 pt.) Determine the absolute...
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= Young's Modulus (psi) I=moment of inertia (in^4) L = Length (in) a=location of point load (in) W = load (lbf)- Objectives We wish to study the deflection as function of x for a given set of system parameters.--To- accomplish this task, we will create two separate M-files. M-file-1 This function-M-file should generate a plot of y...
I need help with this problem.
A cantilever beam is subjected to a linearly distributed load, with W, = 10 kN/m and to an inclined point load F equal to 20 kN, as shown in the figure. The length of the beam is L=10 m. Make a cut at distance x from the free end of the cantilever, as shown in the figure, and use the method of sections to derive expressions for the internal resultant loadings at the cross-section...
Using equation 3 please find the deflection value with the
variables given. Be careful with units please.
P= 10.07 Newtons
L= 953.35 mm
x= 868.363 mm
E= 72.4 GPa
Iy= 5926.62 mm^4
The maximum deflection, WMAX of the cantilever beam occurs at the free end. The magnitude of the deflection may be derived by solving the differential equation: d'w M,(x) P (L-x) eq. 1 dr EI EI where E and Iy are the modulus of elasticity and moment of inertia...
Question 3: A steel (E 30x106 psi and v 0.3) cantilever l-beam is subjected to a distributed load and a concentrated load. The I section is 4-inch-wide and 5-inch-tall, and the flange and web plates are all 0.5-inch-thick, as marked in the figure. a) Draw the moment diagram as a function of x and clearly label the moment values at 1, 2, and 4 ft. (10) b) Find the maximum tensile (normal) stress in the entire beam. (5) c) Find...
ans all parts please
15) (10 Points) Consider a horizontal beam of length L. with uniform cross-section and made out of uniform material. It is resting on the x-axis, with one end at the origin. It is acted upon by a vertical force it's own weight in this simple version). The deflection of the beam at any point x,for 0 <=<L.is given by Ely) = w, where E, I, ware constants. E is the Young's modulus of elasticity of the...
QUESTION 34 The simply supported beam shown in the figure below is subjected to a 3 kN concentrated force. The beam has modulus of elasticity of E-70 GPa and area moment of inertia equals to l-126x10-6 m4 Question 34- Question 38] 3 kN 5 According to successive integration method Ely(x) = x3 (x-2)3 6 12 4 () x2 8 (x+ 1)2 4 QUESTION 36 C2 = 0 QUESTION 36 C2 - 0 2 3 QUESTION 37 C1- 1.33 1.5 2.3...
A steel I-section beam, simply supported at its two ends, is
subjected to a uniformly distributed load q (vertically downward)
over its central segment having a length of 2 m as shown in the
figure. It also shows the type of restraints (F/P/L) against
lateral torsional buckling of the beam at its four sections. The
section at the left end of the beam has only the lateral rotational
restraint. The load is causing bending of the beam about x-x (major...
Review An engineered wood beam (Figure 1) will replace a portion of a structural wall as part of a house renovation. The beam can be modeled as a simply supported beam with a span L = 18 ft and an uniform distributed load w = 810 lb/ft . The beam is to be constructed as an I-beam with nails securing the flanges to the web. The flanges are 6 in wide and 1 in thick. The web has depth 18...