

Study with the several resources on Docsity
Earn points by helping other students or get them with a premium plan
Prepare for your exams
Study with the several resources on Docsity
Earn points to download
Earn points by helping other students or get them with a premium plan
Material Type: Exam; Professor: Geubelle; Class: Finite Element Analysis; Subject: Aerospace Engineering; University: University of Illinois - Urbana-Champaign; Term: Spring 2007;
Typology: Exams
1 / 2
This page cannot be seen from the preview
Don't miss anything!


AE420/ME471 – Spring 2007 – First Midterm Friday, February 23, 2007 50 minutes – Closed notes/closed books/no calculator Question 1: Rayleigh-Ritz Method (7 points) Consider the simple beam buckling problem described in Figure 1.
Figure 1 The beam is of length L , stiffness E and moment of inertia I. It is simply supported at both ends, x=0 and x=L. It is subjected to a compressive axial force P applied at both ends and to a distributed transverse load q(x) (as shown in Figure 1). Note: we only solve for the transverse deflection w , not for the axial displacement. The boundary conditions for this problem are simply
The potential energy for this problem can be shown to be
! =
d^2 w dx^2
2 (
dw dx
2 ( qw
dx 0
L
a) Denoting the approximate deflection solution as
i = 1
N
where the ai are the unknown coefficients and fi are the basis functions, derive the general expression of the
linear system
used to solve the N-component vector A = a 1 a 2 ... aN. Write the matrix [ K ] and vector { R } both in
“matrix/vector” (i.e., [ K ]=…, { R }=…) and component (i.e., Kij =…, Ri =…) forms. What are the
conditions on the basis functions to make them admissible?
b) Assuming N =1, use the simplest polynomial basis function to obtain an approximation for the buckling load for this problem (i.e., the critical value of P for which the deflection w is not zero for zero transverse
Question 2: Assembling (2 points) Consider the simple 2-D truss structure shown in Figure 2. It is composed of 4 nodes and 5 elements. The connectivity table linking nodes to elements is as follows: Element # Node a Node b 1 1 3 2 4 2 3 3 2 4 3 4 5 4 1
q ( x )
Figure 2
Denoting the 16 components of the local stiffness matrix of element m by ki ( j^^ m ), with i and j ranging from 1 to
4, indicate where (i.e., at what row and column) in the stiffness matrix the following components are assembled:
k 12 (^1 ) k 33 (^2 ) k 24 (^4 ) k 23 (^5 )
Question 3: Finite element formulation (11 points) Consider the simple structural problem shown in Figure 3. It consists of a string of length L , with tension T , on an elastic foundation (with distributed stiffness ks ) and subjected to a transverse load q(x). It is attached
a) Starting from the expression of the potential energy for this problem
! =
dw dx
2
0
L
0
L
derive the finite element formulation (i.e., the expression of the local stiffness matrix [ k ] and local load vector { r }) for a generic M - node string element of length l.
b) If M = 3, what is the expression of the shape functions for this element (assuming the second node is in the middle of the element)? Sketch the corresponding shape functions.
c) Knowing that the Principle of Virtual Work (PVW) for this structural problem is
! T dw dx
d " w dx
$%^
L
0
L
derive the finite element formulation using the PVW approach, and compare with the solution found in a).
Figure 3.