Final Exam Problems - Finite Element Analysis | AE 420, Exams of Aerospace Engineering

Material Type: Exam; Professor: Geubelle; Class: Finite Element Analysis; Subject: Aerospace Engineering; University: University of Illinois - Urbana-Champaign; Term: Spring 2007;

Typology: Exams

Pre 2010

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AE420/ME471 – Introduction to the Finite Element Method
Final Exam – Spring 2007
3 hours – Closed notes/closed books/no calculator
Total: 35 points
Problem 1. Theory (7 points)
1. What are the basic idea and the motivation behind the introduction of mapped elements?
2. What is the difference between Euler and Mindlin beam theories? Which beam element locks
and why? What can be done to solve the locking problem and why does it work?
3. Show that the backward difference scheme is always stable for first-order (thermal) transient
problems.
Problem 2. Transient plane stress problem (13 points)
The principle of virtual work (PVW) for a transient plane stress problem is given by
!" #
{ }
d$
$
% +
!
u
&
!!
u
{ }
d$
$
%=
!
u F
{ }
d$
$
% +
!
u T
{ }
d'T
'T
%, (
!
u
{ }
,
where
!
denotes the material density,
u=u x,y,t
( )
v x,y,t
( )
is the (transient) displacement
vector,
T=TxTy
is the (possibly transient) applied traction vector (along the portion
!
T
of
the boundary), and
F=FxFy
is the (possibly transient) body force vector.
The strain
!
{ }
and stress
vectors are defined by
!
{ }
=
"
xx
"
yy
!
xy
#
$
%
&
%
'
(
%
)
%
=
*u/*x
*v/*y
*u/*y+*v/*x
#
$
%
&
%
'
(
%
)
%
,
!
{ }
=
!
xx
!
yy
!
xy
"
#
$
%
$
&
'
$
(
$
=D
[ ]
)
{ }
,
where
is the symmetric 3*3 material stiffness matrix. A superposed dot denotes derivative
with respect to time,
!
u
and
!"
respectively denote the virtual displacement and strain
vectors.
a) Using the PVW approach, derive the semi-discrete finite element formulation for this
problem for a M-node transient plane stress element. Indicate clearly the content of the
vector with the local degrees of freedom. Prior to the derivation of the local stiffness [k]
and mass [m] matrices and of the local load vector {r}, indicate their expected size. Make
sure to provide the complete expression of all quantities used in your derivation.
b) Give the expression of [k], [m] and {r} for the 9-node isoparametric 2D quadrilateral
plane stress element. Write the expression of the shape functions associated with each
node and derive all the quantities entering the expression of [k], [m] and {r} (you do not
need to actually perform the integrations!).
Problem 3. Transient axisymmetric membrane problem (9 points)
The transient transverse deflection
w r,t
( )
of an annular shape membrane of inner and outer radii
a and b, respectively, subjected to a radially varying distributed transient transverse load
q r,t
( )
and supported by an elastic foundation of (constant) distributed stiffness
ks
is described by
pf2

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Download Final Exam Problems - Finite Element Analysis | AE 420 and more Exams Aerospace Engineering in PDF only on Docsity!

AE420/ME471 – Introduction to the Finite Element Method

Final Exam – Spring 2007

3 hours – Closed notes/closed books/no calculator

Total: 35 points

Problem 1. Theory (7 points)

  1. What are the basic idea and the motivation behind the introduction of mapped elements?
  2. What is the difference between Euler and Mindlin beam theories? Which beam element locks

and why? What can be done to solve the locking problem and why does it work?

  1. Show that the backward difference scheme is always stable for first-order (thermal) transient

problems.

Problem 2. Transient plane stress problem (13 points)

The principle of virtual work (PVW) for a transient plane stress problem is given by

!" {# } d $

$

+! u & { u !!} d $

$

=! u { F } d $

$

+! u { T } d '

T

' T

, ({! u } ,

where !denotes the material density, u = u ( x , y , t ) v ( x , y , t ) is the (transient) displacement

vector, T = T x

T

y

is the (possibly transient) applied traction vector (along the portion

T

of

the boundary), and F^ =^ Fx Fy is the (possibly transient) body force vector.

The strain {! }and stress

{! }vectors are defined by

xx

yy

xy

  • u / * x

  • v / * y

  • u / * y + * v / * x

xx

yy

xy

=^ [ D ]{^ ) },

where

[ D ]is the symmetric 3*3 material stiffness matrix. A superposed dot denotes derivative

with respect to time,! u and !" respectively denote the virtual displacement and strain

vectors.

a) Using the PVW approach, derive the semi-discrete finite element formulation for this

problem for a M-node transient plane stress element. Indicate clearly the content of the

vector with the local degrees of freedom. Prior to the derivation of the local stiffness [ k ]

and mass [ m ] matrices and of the local load vector { r }, indicate their expected size. Make

sure to provide the complete expression of all quantities used in your derivation.

b) Give the expression of [ k ], [ m ] and { r } for the 9-node isoparametric 2D quadrilateral

plane stress element. Write the expression of the shape functions associated with each

node and derive all the quantities entering the expression of [ k ], [ m ] and { r } (you do not

need to actually perform the integrations!).

Problem 3. Transient axisymmetric membrane problem (9 points)

The transient transverse deflection w ( r , t )of an annular shape membrane of inner and outer radii

a and b , respectively, subjected to a radially varying distributed transient transverse load q ( r , t )

and supported by an elastic foundation of (constant) distributed stiffness k s

is described by

T

2 w

! r

2

r

! w

! r

( k s

w + q ( r , t ) = )

2 w

! t

2

a * r * b and t > 0

where T is the (constant) tension in the membrane and (^) !is the (constant) surface density of the

membrane. The boundary conditions are assumed to be

w ( r = a , t ) = w

a

( t ) and^ w^ ( r^ =^ b ,^ y ) =^ w

b

( t ),

and the initial conditions assume a quiescent state, i.e.,

w ( r , 0 ) =

! w

! t

( r ,^0 ) =^0 for^ a^ "^ r^ "^ b.

Use the Galerkin Weighted Residual Method (GWRM) to derive the semi-discrete finite element

formulation (stiffness matrix, mass matrix and load vector) for this transient axi-symmetric

membrane problem. Remember that the integration element for an axi-symmetric problem is

2! r dr.

Problem 4. Rayleigh-Ritz Method (6 points)

Consider the beam bending problem shown in the figure below.

The beam is homogeneous and linearly elastic. It has a length L , a moment of inertia I and a

stiffness E. It is cantilever at x = 0 , and is supported by a linear spring (of stiffness k ) at x = L.

The beam is subjected to a uniformly distributed transverse load po (in N/m).

Knowing that the expression of the potential energy for this system is

EI

d

2 w

dx

2

2

dx

0

L

) p o

w dx

0

L

k ( w ( L ))

2 ,

use the RRM to get an approximate expression for the spring deflection.

  1. Get the general form of the linear system for the N unknown coefficients q i

entering the RRM

approximation

w! ( x ) = q

i

f i

( x )

i = 1

N

!^ ,

where f i

( x )denote the basis functions.

  1. Then use the formulation found in step 1) to get the actual approximate solution using the

simplest polynomial basis function.

p o

k

x

z