Using the equations listed on the side, prove that the amount of deflection is given by the equation below:
horizontal velocity imparted=sqrt(2*q*Va/m)
time taken to reach the other end=Dx/speed
=Td=Dx/Vx
time taken to travel distance X=Tf=X/Vx
force along y axis=charge*electric field
=charge*potential difference/distance
=q*Vd/Dy
then acceleration=force/mass
=q*Vd/(Dy*m)
velocity along y axis=acceleration*time
=q*Vd*Td/(Dy*m)
deflection along y axis=velocity*Tf
=q*Vd*Td*tf/(Dy*m)
=q*Vd*Dx*X/(Vx^2*Dy*m)
=q*Vd*Dx*X/(2*q*Va*Dy*m/m)
=Vd*Dx*X/(2*Dy*Va)
hence proved.
Using the equations listed on the side, prove that the amount of deflection is given by...
Determine the deflection, moment and shear diagram equations for
the beam below two ways: (a) using integration of the fourth order
governing differential equation for beams EIv''''=w(x) and (b)
using superposition of known deflections equations for statically
determinate beams provided below.
Thanks
8. For each of the equations listed below, determine the Galois group over Q of the splitting field of the equation. List all of the subgroups of the Galois group. List all of the subfields of the splitting field of the equation, and draw a diagram illustrating the Galois correspondence between subgroups and subfields for each example. a. 2 1) (z2-2) b.(-3) +1) (Note: You must prove by explicit calculation that /3 is not contained in QlV2.) 3
8. For...
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...
Assignment: 25 Marks Using the general stiffness method, calculate the deflection of the free end of the cantilever beam shown in the figure below. Use the slope deflection equations to prove that the moment at the support = 2WL2 and the moment at the position where stiffness changes = 0.5 wite EI Hint: constrain the freedom of movement as indicated 17wL 16 EI Answer:
Assignment: 25 Marks Using the general stiffness method, calculate the deflection of the free end of...
QUESTION 7 22 points (Slope-Deflection) Problem 7. Using Slope-Deflection Method, write all equations using numeric standard decimal values. for calculations (Not Fractions) when known or able to be calculated necessary to solve for the MOMENTS and SLOPES in each span. The support at "A" SETTLES DOWNWARD 0.2 ft. El is constant Assume support at "A" is foed, support "C" is fixed and "B' is a roller. DO NOT SOLVE for the internal moments (22 points 4 kipit 27 36 Ft...
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)...
9. (a)Using the Maxwell's equations prove that the wave equations for the electric and magnetic fields are given by 0t2 where l/c-μοεο
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The deflection of a uniform beam subject to a linearly increasing distributed load can be computed by using the following equation: y = ( 120EIL Given that L 600 cm, I 30,000 cm, wo-2500 N/cm, and E 50,000 KN/cm2 2. Develop a Matlab code that would implement the Golden-Section search method to find the maximum deflection until the error falls below 1% with initial guesses of Xi = 0 and Xu-L. Display all of the following: xl, xu, d, x1...
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...