1. In figure (1), shows a uniform beam subjected to a linear increasing distributed load. The equation for the resulting elastic curve is: w y = 120EIL (-x5+2L²x3 - L*x) Using the numerical methods to determine the point of max. deflection (that is, the value of x where "Y-0. Then substitute dx this value in the given equation to find the value of maximum deflection. Using the following parameter values in your computations: L = 600cm; E50000 k N/cm2;I= 30000cmt and w =2.5 k N/cm. (a) r=Ly- 0) =0, v= 0) (b) Figure (1)

1. In figure (1), shows a uniform beam subjected to a linear increasing distributed load. The equation for the resulting elastic curve is: w y = 120EIL (-x5+2L²x3 - L*x) Using the numerical methods to determine the point of max. deflection (that is, the value of x where "Y-0. Then substitute dx this value in the given equation to find the value of maximum deflection. Using the following parameter values in your computations: L = 600cm; E50000 k N/cm2;I= 30000cmt and w =2.5 k N/cm. (a) r=Ly- 0) =0, v= 0) (b) Figure (1)

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

See similar textbooks

Similar questions

L by the double integeration method. E = 200 GPa , I = 20 X10ʻmm“, and L = 3.0 m._Extra points will be added if you also model it using RISA-2D software. Send me the model file, the deflected shape in a PDF file Compute the values of slope and deflection for the beam shown below at x = with the maximum deflection values, and a screenshot (image) for the deflection value at the pointL shown on the deflected shape. 350 KN/m 70 KN/m 400 KN.m
Consider the beam with properties and loadings as described in the figure and parameter table. Use superposition to find the angles of deflection at A and C (in degrees). M neo 0A = A 0c= 7////////// CC 2022 Cathy Zupke parameter L W BY NC SA Alloy Beam Type value 6 50 65 A992 Steel W310 x 67 O B O units W m kN/m kN m . C
Problem 1: (Please solve parts A and B of problem) A) A uniformly distributed load is subjected on the clamped-clamped beam and it is supported by a spring in the middle of the beam. Using Castigliano’s theorem, find the deflection in the spring. (Please use only Castigliano’s theorem to solve this part) B) Remove the spring in part A and use the Rayleigh-Ritz method to solve for the deflection at the middle of the beam. Assume that v(x) = C (1- Cos((2Pi*x)/L)) (Please use only Rayleigh-Ritz method for this part)
MENG222 Strength of material please I have report lab ((Deflection Measurement for Simply Supported Beam)) Please i need you write ^^^Abstract ^^^ just Abstract please helpe me for that GIVE me good Abstract thank you
A) Calculate the stress in each link when a force of 600 lbs is applied to the rigid element AF, employing manual calculations and finite element methods. B) Determine the corresponding deflection at point A, manually applying the finite element penalty method to model and solve the constraints effectively. Available Data: The links BC and DE are made of steel. Each link has dimensions of 1/2 inch in width and 1/4 inch in thickness. Modulus of elasticity (E): 29 x 10^6 psi. Instructions: For this problem, manual calculation is crucial. Utilize the finite element method with the penalty approach to handle boundary conditions and constraints effectively. This method involves incorporating penalty factors into the system equations to enforce the constraints strictly.
A 0.5kg weight is hung from the end of a cantilever beam, causing a vertical displacement of y = -0.01 inches relative to no load. The weight is increased to 1.0kg. What is the new displacement relative to no load? Typed and correct answer please. I ll rate
Problem 3 For the beam shown in the figure, a) Derive the equation of the elastic curve. b) Compute the rotation at point B. c) Calculate the deflection at point C. Y 2.7 kN.m Y 300 N/m B 3m 3m 3m 3m
Using FE formulation (based on FE element matrices via hand calculations), find the displacement and rotations at the two ends where the diameter changes from 1.5 to 2.0 inches. Provide full stiffness and global matrix.
please read the questıon and slove it again properly.
please solve using CONJUGATE BEAM METHOD
Don't copy from other answers they are wrong , please solve correctly
and y vs. y (phase plot) 4. Consider the deflection v of the beam to the right. The beam is supported at each end and sags due to its own weight (a distributed load q = 50 kN/m). The equation describing the deflection is d'u qx (x- L) dx 2EI where L=5.0 m, I = 0.0052 m* and E = 1.0x1010 Pa. Use the method of your choosing (shooting or finite differences) to solve for: 1) the slope at each end of the beam; 2) the maximum deflection; and 3) the location of maximum deflection.