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MANE 4240 & CIVL 4240 Introduction to Finite Elements Principles of minimum potential energy and Rayleigh- Ritz Prof. Suvranu De

MANE 4240 & CIVL 4240 Introduction to Finite Elements

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MANE 4240 & CIVL 4240 Introduction to Finite Elements. Prof. Suvranu De. Principles of minimum potential energy and Rayleigh-Ritz. Reading assignment: Section 2.6 + Lecture notes. Summary: Potential energy of a system Elastic bar String in tension Principle of Minimum Potential Energy - PowerPoint PPT Presentation

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Page 1: MANE 4240 & CIVL 4240 Introduction to Finite Elements

MANE 4240 & CIVL 4240Introduction to Finite Elements

Principles of minimum potential energy and

Rayleigh-Ritz

Prof. Suvranu De

Page 2: MANE 4240 & CIVL 4240 Introduction to Finite Elements

Reading assignment:

Section 2.6 + Lecture notes

Summary:• Potential energy of a system

•Elastic bar•String in tension

•Principle of Minimum Potential Energy•Rayleigh-Ritz Principle

Page 3: MANE 4240 & CIVL 4240 Introduction to Finite Elements

A generic problem in 1D

11

00

10;02

2

xatu

xatu

xxdx

ud

Approximate solution strategy:GuessWhere o(x), 1(x),… are “known” functions and ao, a1, etc are constants chosen such that the approximate solution 1. Satisfies the boundary conditions2. Satisfies the differential equation

Too difficult to satisfy for general problems!!

...)()()()( 22110 xaxaxaxu o

Page 4: MANE 4240 & CIVL 4240 Introduction to Finite Elements

Potential energy

Wloadingofenergypotential(U)energyStrain

The potential energy of an elastic body is defined as

Page 5: MANE 4240 & CIVL 4240 Introduction to Finite Elements

F

uF

x

k

ku

k

1

Hooke’s LawF = ku

Strain energy of a linear spring

F = Force in the spring u = deflection of the springk = “stiffness” of the spring

Page 6: MANE 4240 & CIVL 4240 Introduction to Finite Elements

Strain energy of a linear spring

F

u u+du

Differential strain energy of the spring for a small change in displacement (du) of the spring

FdudU For a linear spring

kududU

The total strain energy of the spring

2u

0uk

2

1duukU

dU

Page 7: MANE 4240 & CIVL 4240 Introduction to Finite Elements

Strain energy of a nonlinear spring

F

u u+du

FdudU The total strain energy of the spring

curventdispalcemeforcetheunderAreaduFUu

0

dU

Page 8: MANE 4240 & CIVL 4240 Introduction to Finite Elements

Potential energy of the loading (for a single spring as in the figure)

FuW

Potential energy of a linear spring

Wloadingofenergypotential(U)energyStrain

Fuku2

1Π 2

F

x

k

ku

Example of how to obtain the equlibr

Page 9: MANE 4240 & CIVL 4240 Introduction to Finite Elements

Principle of minimum potential energy for a system of springs

For this system of spring, first write down the total potential energy of the system as:

3x2

2322

21 Fd)dd(k2

1)d(k

2

1

xxxsystem

Obtain the equilibrium equations by minimizing the potential energy

1k Fx

2k

1xd2xd 3xd

)2(0)dd(kd

)1(0)dd(kdkd

2323

232212

EquationF

Equation

xxx

system

xxxx

system

Page 10: MANE 4240 & CIVL 4240 Introduction to Finite Elements

Principle of minimum potential energy for a system of springs

In matrix form, equations 1 and 2 look like

Fx

x 0

d

d

kk

kkk

3

2

22

221

Does this equation look familiar?

Also look at example problem worked out in class

Page 11: MANE 4240 & CIVL 4240 Introduction to Finite Elements

Axially loaded elastic bar

x

y

x=0 x=L

A(x) = cross section at xb(x) = body force distribution (force per unit length)E(x) = Young’s modulusu(x) = displacement of the bar at x

x

F

dx

duε Axial strain

Axial stressdx

duEEε

Strain energy per unit volume of the bar2

dx

duE

2

1σε

2

1dU

Strain energy of the bar

Adxσε2

1dVσε

2

1dUU

L

0x since dV=Adx

Page 12: MANE 4240 & CIVL 4240 Introduction to Finite Elements

Axially loaded elastic bar

Strain energy of the bar

LL

0

2

0dx

dx

duEA

2

1dxσεA

2

1U

Potential energy of the loading

L)Fu(xdxbuW0

L

Potential energy of the axially loaded bar

L)Fu(xdxbudxdx

duEA

2

100

2

LL

Page 13: MANE 4240 & CIVL 4240 Introduction to Finite Elements

Principle of Minimum Potential EnergyAmong all admissible displacements that a body can have, the one that minimizes the total potential energy of the body satisfies the strong formulation

Admissible displacements: these are any reasonable displacement that you can think of that satisfy the displacement boundary conditions of the original problem (and of course certain minimum continuity requirements). Example:

Exact solution for the displacement field uexact(x)

Any other “admissible” displacement field w(x)

L0x

Page 14: MANE 4240 & CIVL 4240 Introduction to Finite Elements

Lets see what this means for an axially loaded elastic bar

A(x) = cross section at xb(x) = body force distribution (force per unit length)E(x) = Young’s modulusx

y

x=0 x=Lx

F

Potential energy of the axially loaded bar corresponding to the exact solution uexact(x)

L)(xFudxbudxdx

duEA

2

1)(u exact0 exact0

2

exactexact

LL

Page 15: MANE 4240 & CIVL 4240 Introduction to Finite Elements

Potential energy of the axially loaded bar corresponding to the “admissible” displacement w(x)

L)Fw(xdxbwdxdx

dwEA

2

1(w)

00

2

LL

Exact solution for the displacement field uexact(x)

Any other “admissible” displacement field w(x)

L0x

Page 16: MANE 4240 & CIVL 4240 Introduction to Finite Elements

Example:

Lxbdx

udAE 0;0

2

2

LxatFdx

duEA

xatu

00

Assume EA=1; b=1; L=1; F=1Analytical solution is

22

2xxuexact

6

71)(xudxudx

dx

du

2

1)(u exact

1

0 exact

1

0

2

exactexact

Potential energy corresponding to this analytical solution

Page 17: MANE 4240 & CIVL 4240 Introduction to Finite Elements

Now assume an admissible displacement

xw Why is this an “admissible” displacement? This displacement is quite arbitrary. But, it satisfies the given displacement boundary condition w(x=0)=0. Also, its first derivate does not blow up.

11)w(xdxwdxdx

dw

2

1(w)

1

0

1

0

2

Potential energy corresponding to this admissible displacement

Notice

(w))(u

16

7

exact

since

Page 18: MANE 4240 & CIVL 4240 Introduction to Finite Elements

Principle of Minimum Potential EnergyAmong all admissible displacements that a body can have, the one that minimizes the total potential energy of the body satisfies the strong formulation

Mathematical statement: If ‘uexact’ is the exact solution (which satisfies the differential equation together with the boundary conditions), and ‘w’ is an admissible displacement (that is quite arbitrary except for the fact that it satisfies the displacement boundary conditions and its first derivative does not blow up), then (w))(uexact

unless w=uexact (i.e. the exact solution minimizes the potential energy)

Page 19: MANE 4240 & CIVL 4240 Introduction to Finite Elements

he Principle of Minimum Potential Energy and the strong formulation are exactly equivalent statements of the same problem.

The exact solution (uexact) that satisfies the strong form, renders the potential energy of the system a minimum.

So, why use the Principle of Minimum Potential Energy?The short answer is that it is much less demanding than the strong formulation. The long answer is, it1. requires only the first derivative to be finite2. incorporates the force boundary condition automatically. The admissible displacement (which is the function that you need to choose) needs to satisfy only the displacement boundary condition

Page 20: MANE 4240 & CIVL 4240 Introduction to Finite Elements

Finite element formulation, takes as its starting point, not the strong formulation, but the Principle of Minimum Potential Energy.

Task is to find the function ‘w’ that minimizes the potential energy of the system

From the Principle of Minimum Potential Energy, that function ‘w’ is the exact solution.

L)Fw(xdxbwdxdx

dwEA

2

1(w)

00

2

LL

Page 21: MANE 4240 & CIVL 4240 Introduction to Finite Elements

Step 1. Assume a solution

...)()()()( 22110 xaxaxaxw o

Where o(x), 1(x),… are “admissible” functions and ao, a1, etc are constants to be determined from the solution.

Rayleigh-Ritz Principle

The minimization of the potential energy is difficult to perform exactly.The Rayleigh-Ritz principle is an approximate way of doing this.

Page 22: MANE 4240 & CIVL 4240 Introduction to Finite Elements

Step 2. Plug the approximate solution into the potential energy

L)Fw(xdxbwdxdx

dwEA

2

1(w)

00

2

LL

Rayleigh-Ritz Principle

...)()(F

dx...b

dx...dx

d

dx

dEA

2

1,...)a,(a

1100

0 1100

0

2

11

0010

LxaLxa

aa

aa

L

L

Page 23: MANE 4240 & CIVL 4240 Introduction to Finite Elements

Step 3. Obtain the coefficients ao, a1, etc by setting

,...2,1,0,0(w)

iai

Rayleigh-Ritz Principle

The approximate solution is

...)()()()( 22110 xaxaxaxu o

Where the coefficients have been obtained from step 3

Page 24: MANE 4240 & CIVL 4240 Introduction to Finite Elements

Example of application of Rayleigh Ritz Principle

x

x=0 x=2x=1

FE=A=1F=2

1

2

0

2

1)Fu(xdxdx

du

2

1(u)

xatappliedFloadofEnergyPotential

EnergyStrain

The potential energy of this bar (of length 2) is

Let us assume a polynomial “admissible” displacement field2

210u xaxaa

Note that this is NOT the analytical solution for this problem.

Page 25: MANE 4240 & CIVL 4240 Introduction to Finite Elements

Example of application of Rayleigh Ritz Principle

For this “admissible” displacement to satisfy the displacement boundary conditions the following conditions must be satisfied:

0422)u(x

00)u(x

210

0

aaa

a

Hence, we obtain

21

0

2

0

aa

a

Hence, the “admissible” displacement simplifies to

22

2210

2

u

xxa

xaxaa

Page 26: MANE 4240 & CIVL 4240 Introduction to Finite Elements

Now we apply Rayleigh Ritz principle, which says that if I plug this approximation into the expression for the potential energy , I can obtain the unknown (in this case a2) by minimizing

4

3

023

8

0

23

4

2Fdx2dx

d

2

1

1)Fu(xdxdx

du

2

1(u)

2

2

2

22

2

1

22

2

0

22

2

2

0

2

a

a

a

aa

xxaxxaxat

evaluated

Page 27: MANE 4240 & CIVL 4240 Introduction to Finite Elements

2

22

2210

24

3

2

u

xx

xxa

xaxaa

Hence the approximate solution to this problem, using the Rayleigh-Ritz principle is

Notice that the exact answer to this problem (can you prove this?) is

212

10uexact xforx

xforx

Page 28: MANE 4240 & CIVL 4240 Introduction to Finite Elements

0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8 20

0.2

0.4

0.6

0.8

1

x

Exact solution

Approximatesolution

The displacement solution :

How can you improve the approximation?

Page 29: MANE 4240 & CIVL 4240 Introduction to Finite Elements

0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8 2

-1.5

-1

-0.5

0

0.5

1

1.5

x

Str

ess

Approximatestress

Exact Stress

The stress within the bar: