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Material Type: Exam; Professor: Geubelle; Class: Finite Element Analysis; Subject: Aerospace Engineering; University: University of Illinois - Urbana-Champaign; Term: Spring 2007;
Typology: Exams
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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)
and why? What can be done to solve the locking problem and why does it work?
problems.
Problem 2. Transient plane stress problem (13 points)
The principle of virtual work (PVW) for a transient plane stress problem is given by
$
$
$
T
' T
vector, T = T x
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.
xx
yy
xy
u / * x
v / * y
u / * y + * v / * x
xx
yy
xy
where
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)
and supported by an elastic foundation of (constant) distributed stiffness k s
is described by
2 w
! r
2
r
! w
! r
( k s
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
a
b
and the initial conditions assume a quiescent state, i.e.,
! w
! t
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
d
2 w
dx
2
2
dx
0
L
) p o
w dx
0
L
2 ,
use the RRM to get an approximate expression for the spring deflection.
entering the RRM
approximation
i
f i
i = 1
N
where f i
simplest polynomial basis function.
p o
k
x
z