P L The deformation of a simply supported beam under a distributed load p, shown in the figure above, is governed by the equation d'y M(x) dx² EI where M(x) is the internal bending moment and is given by px(L-x) M(x)= 2 y(x) = C, X Other relevant data are E=29×10° lb/in², I = 3100 in, L=20 ft = 240 in, p=5000 lb/ft 5000 lb/(12 in). 1) Obtain the exact solution by integration, and find the maximum deflection y max. 2) Assume an approximate deflection solution of the form (주)-( Note that the proposed form satisfies the boundary conditions. Use the following methods to evaluate C₁ and calculate the maximum deflection ymax: (a) the collocation method (using the midpoint of the beam for collocation); (b) the subdomain method; (c) Galerkin's method. Compare the approximate results with exact solution. 3) Draw the exact solution and approximate solutions obtained from 2) on one figure (as Figure 2-4 in lecture 2 shows) to show how exaction and approximate solutions look like and are different from one another. Comment on the solutions ontained using different methods.
P L The deformation of a simply supported beam under a distributed load p, shown in the figure above, is governed by the equation d'y M(x) dx² EI where M(x) is the internal bending moment and is given by px(L-x) M(x)= 2 y(x) = C, X Other relevant data are E=29×10° lb/in², I = 3100 in, L=20 ft = 240 in, p=5000 lb/ft 5000 lb/(12 in). 1) Obtain the exact solution by integration, and find the maximum deflection y max. 2) Assume an approximate deflection solution of the form (주)-( Note that the proposed form satisfies the boundary conditions. Use the following methods to evaluate C₁ and calculate the maximum deflection ymax: (a) the collocation method (using the midpoint of the beam for collocation); (b) the subdomain method; (c) Galerkin's method. Compare the approximate results with exact solution. 3) Draw the exact solution and approximate solutions obtained from 2) on one figure (as Figure 2-4 in lecture 2 shows) to show how exaction and approximate solutions look like and are different from one another. Comment on the solutions ontained using different methods.
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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Transcribed Image Text:y
نیستی
Р
▬▬▬▬▬▬▬▬▬▬
L
The deformation of a simply supported beam under a distributed load p, shown in the figure
above, is governed by the equation
d²y__M(x)
EI
dx²
where M(x) is the internal bending moment and is given by
M(x) =
px(L-x)
2
X
Other relevant data are E=29×10° lb/in², I = 3100 in¹, L=20 ft = 240 in, p=5000
lb/ft=5000 lb/(12 in).
1) Obtain the exact solution by integration, and find the maximum deflection y max.
2) Assume an approximate deflection solution of the form
X
y(x) = c [(i)* - (
Note that the proposed form satisfies the boundary conditions. Use the following methods to
evaluate C₁ and calculate the maximum deflection ymax: (a) the collocation method (using
the midpoint of the beam for collocation); (b) the subdomain method; (c) Galerkin's method.
Compare the approximate results with exact solution.
3) Draw the exact solution and approximate solutions obtained from 2) on one figure (as
Figure 2-4 in lecture 2 shows) to show how exaction and approximate solutions look like and
are different from one another. Comment on the solutions ontained using different methods.
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