THEORY OF ELASTICITY & PLASTICITY
NUMERICAL PROBLEM
Done by: Ashwani Jha
Question: Find the approximate deflection of a simply supported beam carrying
a symmetrical Triangular load P using Rayleigh Ritz method.
Solution:
Let w(x) denote the deflection of the beam(field variable).The differential
equation formulation leads to following statement of the problem:
i.e it satisfies the governing equation
. /
And the boundary conditions
{
( ) ( )
( ) ( ) ( ) ( )
}
P
Total energy i.e. potential energy of the system is given below:
Π= ∫ [ ( ) ( )]
Replace P=8
( )
( )
( )
9
Π= [∫ { ( ) ( )} ∫ { ( ) (
( )
)} ]
Where E=Young’s Modulus
I=Moment of inertia, l=length of beam, P=load on beam
Now we are integrating above equation denoted in different color
separately.
Let here w(x)=
( ) ( ) , where C1 and C2 are constant
After using the value of and w in above equation we have,
∫ 0 ( ( ) ( ) ) .
( )
/1
∫ 6 2 ( ) ( ) ( ) ( ) ( ) ( ) 3
4
( )
57 ( )
We know that, ∫ 2 3
∫
Therefore, equation (1) becomes
2 ( ) ( ) 3 ∫ 64
( )
57
2 ( ) ( ) 3 ∫ 64
( )
57 ( )
∫ [ ∫ ∫ ( ) ]
[ ∫ ( ) ]
0 ( ) ( )1
0( ) 1
Similarly
∫ ( )
Now equation (2) becomes
2 ( ) ( ) 3 0 ( ) ( ) 1 ( )
∫ * ( ) (
( )
)+ = ∫ * ( ) ( )+
∫ 6 . / 8 ( )
( )
97
∫ [ ∫ ∫ ( ) ]
[ ∫ ( ) ]
[ ∫ ( ) ]
[ ( ) ]
Similarly,
∫ 0 ( ) 1
Therefore, I2 now becomes after substituting the value
{ ( ) ( ) } , - 0 2 ( ) 3
{ ( ) }1…… (4)
Therefore, Π= [ ]
i.e. Π= 0 , ( ) ( ) - * ( ) ( ) + , ( )
( ) - , - * , ( ) - , ( ) -+1
where C1 and C2 are independent constant. For the minimum of π we have
{ ( ) } , - =0
{ ( ) }=0
Therefore,
( ) , which is the deflection of beam.
The deflection of beam at the middle point of beam(i.e. at l/2) is given by
( ) ( )
which compare with the exact solution
( ) ( )

FEM problem of elasticity

  • 1.
    THEORY OF ELASTICITY& PLASTICITY NUMERICAL PROBLEM Done by: Ashwani Jha
  • 2.
    Question: Find theapproximate deflection of a simply supported beam carrying a symmetrical Triangular load P using Rayleigh Ritz method. Solution: Let w(x) denote the deflection of the beam(field variable).The differential equation formulation leads to following statement of the problem: i.e it satisfies the governing equation . / And the boundary conditions { ( ) ( ) ( ) ( ) ( ) ( ) } P
  • 3.
    Total energy i.e.potential energy of the system is given below: Π= ∫ [ ( ) ( )] Replace P=8 ( ) ( ) ( ) 9 Π= [∫ { ( ) ( )} ∫ { ( ) ( ( ) )} ] Where E=Young’s Modulus I=Moment of inertia, l=length of beam, P=load on beam Now we are integrating above equation denoted in different color separately. Let here w(x)= ( ) ( ) , where C1 and C2 are constant After using the value of and w in above equation we have, ∫ 0 ( ( ) ( ) ) . ( ) /1 ∫ 6 2 ( ) ( ) ( ) ( ) ( ) ( ) 3 4 ( ) 57 ( )
  • 4.
    We know that,∫ 2 3 ∫ Therefore, equation (1) becomes 2 ( ) ( ) 3 ∫ 64 ( ) 57 2 ( ) ( ) 3 ∫ 64 ( ) 57 ( ) ∫ [ ∫ ∫ ( ) ] [ ∫ ( ) ] 0 ( ) ( )1 0( ) 1 Similarly ∫ ( ) Now equation (2) becomes
  • 5.
    2 ( )( ) 3 0 ( ) ( ) 1 ( ) ∫ * ( ) ( ( ) )+ = ∫ * ( ) ( )+ ∫ 6 . / 8 ( ) ( ) 97 ∫ [ ∫ ∫ ( ) ] [ ∫ ( ) ] [ ∫ ( ) ] [ ( ) ] Similarly, ∫ 0 ( ) 1 Therefore, I2 now becomes after substituting the value { ( ) ( ) } , - 0 2 ( ) 3 { ( ) }1…… (4)
  • 6.
    Therefore, Π= [] i.e. Π= 0 , ( ) ( ) - * ( ) ( ) + , ( ) ( ) - , - * , ( ) - , ( ) -+1 where C1 and C2 are independent constant. For the minimum of π we have { ( ) } , - =0 { ( ) }=0 Therefore, ( ) , which is the deflection of beam. The deflection of beam at the middle point of beam(i.e. at l/2) is given by ( ) ( ) which compare with the exact solution
  • 7.