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Advanced Mechanics - Solved Assignments and Essays

The assignment requires students to apply advanced knowledge, scientific and mathematical principles to model a mechanical system, critically apply and integrate knowledge from other engineering disciplines, identify and describe the performance of systems and components using analytical methods, and develop an understanding of vibration and its application to industrial plant and machinery.

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Added on  2023-04-25

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Advanced Mechanics - Solved Assignments and Essays

The assignment requires students to apply advanced knowledge, scientific and mathematical principles to model a mechanical system, critically apply and integrate knowledge from other engineering disciplines, identify and describe the performance of systems and components using analytical methods, and develop an understanding of vibration and its application to industrial plant and machinery.

   Added on 2023-04-25

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ADVANCED MECHANICS
ADVANCED MECHANICS
Name of the Student
Name of the University
Author Note
Advanced Mechanics - Solved Assignments and Essays_1
1ADVANCED MECHANICS
Question 1:
The diagram of the beam is given below.
The beam AB is hinged at the end A and is being vertically supported at the other end B.
The applied force is distributed triangular force f(x) = f0*(x/L) (x is the positive horizontal
co-ordinate from the point A). The point A is taken as origin of the co-ordinate.
a) The reaction forces at the supporting points A and B are equal to vertical forces applied to
those points.
Reaction force at A or at length x=0 (RA) = f0*(0/L) = 0 kN.
Reaction force at B or at length x=L (RB) = f0*(L/L) = f0 kN.
b) and c) Now, the deflection equation of the beam will be
EI
( d4 y
d x4 )=f 0( x
L )
The separating the variable and integrating the equation becomes
Advanced Mechanics - Solved Assignments and Essays_2
2ADVANCED MECHANICS
EIy
( d2 y
d x2 )=f 0( x3
6 L )+ C 1x +C 2........(1)
Now, again separating the variables and then integrating twice we get
EI*y = f 0( x5
120 L )+C 1x3
6 +C 2x2
2 +C 3x +C 4.....(2)
Now, the equation (1) is the bending moment equation and the equation (2) is the deflection
equation.
Now, applying the boundary conditions at x = 0 and at x= L both moment and deflection
vanish.
Hence, the constants of the equation are
C1 = f0*L/6, C2 = 0, C3 = -7*f0(L^3)/360, C4 = 0.
Substituting the values in the equation (2) gives
y= ( f 0x
360 LEI ) ( 7 L4 10 L2 x2
+3 x4 )
Now, Moment Mx=EI
( d2 y
d x2 )
Hence, the expression of moment from equation (1) will be
yMx=f 0( x3
6 L )+(f 0L
6 )x
Mx=f 0( x3
6 yL )+(f 0L
6 y )x......(3)
The equation (3) is the moment deflection equation.
Now, putting the values of constants in the equation (2) we get the equation of deflection.
Advanced Mechanics - Solved Assignments and Essays_3

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