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Explicit and Implicit Analysis Aim: To use the given equation and solve…
Chandrababu Reddy R
updated on 15 May 2021
Explicit and Implicit Analysis
Aim: To use the given equation and solve using both Explicit and Implicit Methods
Introduction:
The finite element method is a numerical technique for obtaining approximate solution to a wode variety engineering problems. FEA (Finite Element Analysis) has done by three phases.
1. Pre-processing
2. Solution
3. post-Processing
Sloving the problems systematically yields equations and attempts to approximate the values of the unknowns. This method subdivides the overall problem into simpler sub-issues that are easier to solve. In turn, these sub-issues called finite elements require implicit vs explicit analysis. All of these implicit vs explicit problems are expressed through mathematical partial differential equations
Explicit analysis: An Explicit FEM analysis does the incremental procedure and at the end of each increment updates the stiffness matrix based on geometry changes and material changes. In this type of analysis if the increments are small enough the results will be accurate.
To calculate the displacement every time we have to refer previous data. to solve a mathematical problem Explicit analysis is time dependent that is time step is very small so that effects of acceleration cannot be neglected. Explicit analysis involve mass matrix inversion. In this type the deformation is large because of velocity, acceleration with mass and inertia. cost per time step is less because time taken to slove dynamic problems are less. parallel processing is not posible. The Explicit method should be used when the effects of strain rates are more such are crash, impact test.
Implicit analysis: An Implicit FEM analysis is the same as Explicit with the addition that after each increment the analysis does Newton-Raphson iterations to enforce equilibrium of the internal structure forces with the externally applied loads.
Implicit methods find a solution by solving an equation involving both the current state of the system and the later one. to solve a mathematical problem Implicit analysis is time independent that is time step is large so that effects of acceleration are neglected. Implicit analysis involve stiffness matrix inversion.
in this type the deformation is small because involves in pure force. cost per time step is large because time taken to slove dynamic problems are more. parallel processing is posible. The implicit method should be used when the events are much slower and the effects of strain rates are minimal.
Calculations
Explicit analysis:
Given function f(u)=u3+9u2+4u use this equation and solve using both Explicit and Implicit Methods
The given function 'F(u) is the function of displacement 'u' ehich is given by
f(u)=u3+9u2+4u eq1
to get stiffness diffrencitating force F wrt to displacement u so that we can get stiffness (K = force /deformation)
K(u)=dFdu=3u2+18u+4 eq 2
We have F = Ku - eq3 from the stiffness equation
here the force is ΔF and displacement Δu
So we can return eq 2 as
ΔF=K⋅Δu eq4
Step 1
When there is no deformation that is initial condation u0=0 substitute in eq 2 and 2
f(u0)=0
K(u)=dFdu=3u2+18u+4
K(u0)=3X0+18X0+4,K(u0)=4
For this example three equal load increments (or steps) of ∆F = 1 unit each are used to load the tension bar.
when ΔF=1 duve to extranal force there will be deformation so from the equation 4
Δu1=ΔFK(u0)=14=0.25
u1=u0+Δu1
u1=0+0.25
u1=0.25
Step 2
consider u=u1=0.25 and load increments (or steps) of ∆F = 1
K(u1)=3(0.25)2+18(0.25)+4
K(u1)=8.69
Δu1=ΔFK(u1)=18.69=0.115
u2=u1+Δu2
u2=0.25+0.115
u1=0.365
Step 3
consider u=u2=0.365 and load increments (or steps) of ∆F =1`
K(u2)=3(0.365)2+18(0.365)+4
K(u2)=10.97
Δu2=ΔFK(u2)=110.97=0.091
u3=u2+Δu2
u2=0.365+0.0911
u1=0.456
So from the above force extranl is given by 3 times of applied step load in every instant.
Fexternal=ΔF+ΔF+ΔF=1+1+1+=3
And the force produced internal due to extranal force for every step is given by
f(Internal)1=u31+9u21+4u1=0.253+9(0.252)+4(0.25)=1.578
f(Internal)2=u32+9u22+4u2=0.3653+9(0.3652)+4(0.365)=2.707
f(Internal)3=u33+9u23+4u3=0.4563+9(0.4562)+4(0.456)=3.79
Step i | ΔFi | Δui | ui | (Fexternal)i | (fInternal)i | (fInternal)i−(Fexternal)i=R |
1 | 1 | 0.25 | 0.25 | 1 | 1.578 | 0.578 |
2 | 1 | 0.115 | 0.365 | 2 | 2.707 | 0.707 |
3 | 1 | 0.091 | 0.456 | 3 | 3.79 | 0.79 |
Implicit analysis:
An implicit analysis is the same as the explicit analysis, except that at the end of each step Newton-Raphson iterations are used to enforce equilibrium before moving to the next step.
δuj+1=−[k(uj)]]−1Rj.
The implicit analysis proceeds as follows (results are approximate,they are more precise if done in a computer to machine precision)
Step 1
When there is no deformation that is initial condation u0=0 substitute in eq 2 and 2
f(u0)=0
K(u)=dFdu=3u2+18u+4
K(u0)=3X0+18X0+4,K(u0)=4
For this example three equal load increments (or steps) of ∆F = 1 unit each are used to load the tension bar.
when ΔF=1 duve to extranal force there will be deformation so from the equation 4
Δu1=ΔFK(u0)=14=0.25
u1=u0+Δu1
u1=0+0.25
u1=0.25
Check the residual
Fexternal = ΔF=1
f(Internal)1=u31+9u21+4u1=0.253+9(0.252)+4(0.25)=1.578
R0=(fInternal)i−(Fexternal)i
R0=1.578−1=0.578>10−2 Newton-Raphson iterations are necessary
Calculate the correction to u1=u01
δuj+1=−[k(uj)]]−1Rj. where j=0`
δu1=−[k(u01)]]−1R0
K(u1)=3X0.252+18X0.25+4,K(u1)=8.687
δu1=−[8.687]−1⋅0.578=−0.066
The updated value of u11=u01+δu1
u11=0.25−0.066=0.184
Check the residual again,
Fexternal = ΔF=1
f(Internal)1=(u11)3+9(u11)2+4u11=0.1843+9(0.1842)+4(0.184)=1.046
R1=(fInternal)i−(Fexternal)i
R1=1.046−1=0.046>10−2 Newton-Raphson iterations are necessary`
Calculate the correction to u1=u11
δuj+1=−[k(uj)]]−1Rj. where j=1`
δu2=δu1−[k(u11)]]−1R1
K(u2)=3X0.1842+18X0.184+4,K(u2)=7.41
δu1=−0.066−[7.41]−1⋅0.046=−0.0722
The updated value of u21=u01+δu2
u21=0.25−0.0722=0.177
Check the residual again,
Fexternal = ΔF=1
f(Internal)1=(u21)3+9(u21)2+4u21=0.1773+9(0.1772)+4(0.177)=0.995
R2=(fInternal)i−(Fexternal)i
R2=0.995−1=−0.005<10−2 no further iterations are necessary.
hence the value of u1=0.177
Step 2
u1=0.177
K(u)=dFdu=3u2+18u+4
K(u1)=3X0.1772+18X0.177+4,K(u0)=7.27
Δu2=ΔFK(u0)=17.27=0.137
u2=u1+Δu2
u2=0.177+0.137
u2=0.314
Check the residual
Fexternal = ΔF=2
f(Internal)2=u32+9u22+4u2=0.3143+9(0.3142)+4(0.314)=2.174
R0=(fInternal)i−(Fexternal)i
R0=2.174−2=0.174>10−2 `Newton-Raphson iterations are necessary
Calculate the correction to u2=u02
δuj+1=−[k(uj)]]−1Rj. where j=0`
δu1=−[k(u02)]]−1R0
K(u2)=3X0.3142+18X0.314+4,K(u1)=9.9477
δu1=−[9.947]−1⋅0.174=−0.017
The updated value of u12=u02+δu1
u12=0.314−0.0174=0.296
Check the residual again,
Fexternal = ΔF=2
f(Internal)2=(u12)3+9(u12)2+4u12=0.2963+9(0.2962)+4(0.296)=1.9984
R1=(fInternal)i−(Fexternal)i
R1=1.9984−2=−0.0015<10−2no further iterations are necessary.
hence the value of u2=0.296
Step 3
u_2=0.296`
K(u)=dFdu=3u2+18u+4
K(u2)=3X0.2962+18X0.296+4,K(u2)=9.59
Δu3=ΔFK(u2)=19.59=0.104
u3=u2+Δu3
u2=0.296+0.104
u3=0.4
Check the residual
Fexternal = ΔF=3
f(Internal)3=u33+9u23+4u3=0.43+9(0.42)+4(0.4)=3.104
R0=(fInternal)i−(Fexternal)i
R0=3.104−3=0.104>10−2 `Newton-Raphson iterations are necessary
Calculate the correction to u3=u03
δuj+1=−[k(uj)]]−1Rj. where j=0`
δu1=−[k(u03)]]−1R0
K(u3)=3X0.42+18X0.4+4,K(u1)=11.68
δu1=−[11.68]−1⋅0.104=−0.0089
The updated value of u13=u03+δu1
u13=0.4−0.0089=0.391
Check the residual again,
Fexternal = ΔF=3
f(Internal)3=(u13)3+9(u13)2+4u13=0.3913+9(0.3912)+4(0.391)=2.999
R1=(fInternal)i−(Fexternal)i
R1=2.999−3=−0.00029<10−2no further iterations are necessary.
hence the value of u2=0.391
Step i | ΔFi | Δui | ui | (Fexternal)i | (fInternal)i | (fInternal)i−(Fexternal)i=R |
1 | 1 | 0.25 | 0.177 | 1 | 0.995 | -0.005 |
2 | 1 | 0.137 | 0.296 | 2 | 1.998 | -0.0015 |
3 | 1 | 0.104 | 0.391 | 3 | 2.999 | -0.00029 |
Results: To use the given equation and solve using both Explicit and Implicit Methods is done and comparison results are plotted.
In the plot below the comparison done on Exact , Explicit and Implicit, where Explicit analysis is deveating from the exact solution this is beacuse of lack of equilibrium between the internal and external forces.
In order to achive the sulution near to exact the an implicit analysis is required. The results for the implicit analysis are shown in the below plot. Because of The Newton-Raphson iterations correct we achived the solution which almost equal to the exact solution.
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