Name: _
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EGM 3601 EXAM #1
SUMMER 2014
June 3rd, 2014
8:00 AM 9:50 AM
Instructions:
1. To obtain maximum credit for a problem, you must present your solution clearly.
Accordingly:
a. Wherever appropriate, free body diagrams must be d

Name:
Student No.
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(print legibly)
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University of Central Florida
EGM 3601 SolidIvli:lXil.', Spring 2013
Instructor: Dr. Yuanli Bai (ENGR. l" Room 214, (407) 823-4548, [email protected] )
Date: Monday, April 29th, 2013,7:00am - 9:50am
INS

EGM 3601 Solid Mechanics
Lecture 04: Stress and Strain Relationship
Dr. Yuanli Bai, Assistant Professor
Department of Mechanical, Materials and Aerospace Engineering
University of Central Florida
EGM 3601 Solid Mechanics
1
Recall: Stress and Strain
P
A
No

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EGM 3601 EXAM #1
SUMMER 2013
June 10th, 2013
8:00 AM 9:50 AM
Instructions:
1. To obtain maximum credit for a problem, you must present your solution clearly.
Accordingly:
a. Wherever appropriate, free body diagrams must be

A non circular tube, with
the cross section in blue,
will have some external
torque applied to it. For
the given dimensions,
determine the area A.
2.30"
2.30"
2.25"
2.25"
A non circular tube, with
the cross section in blue,
is subject to a torque of
325 i

UNIVERSITY of CENTRAL FLORIDA
COLLEGE OF ENGINEERING and COMP. SCIENCE
EGN 3343-002: THERMDYNAMICS
Spring 2016
INSTRUCTOR: Ramesh D. Bhavsar, Ph.D.
Office: ENG 1 - 345
Contact Nos: 407 923 7870 / 321 765 4744
e- mail: [email protected]
OFFICE HRS: Tu

EGM3601SolidMechanics
Strain Transformation
Chapter 10
Mechanical and Aerospace
Engineering
TransformationofPlaneStrain
Plane strain - deformations of the material
take place in parallel planes and are the
same in each of those planes.
Fig. 7.47 Plane st

EGM3601SolidMechanics
Design of Beams and Shafts
Chapter 11
Mechanical and Aerospace
Engineering
DesignofBeamsandShafts
1. How to design beams and shafts that would be able to
resist both internal bending and shear?
2. We will look for a method for determ

EGM3601SolidMechanics
Stress Transformation
Chapter 9
Mechanical and Aerospace
Engineering
Introduction
The most general state of stress at a point may
be represented by 6 components,
x , y , z
normal stresses
xy , yz , zx
shearing stresses
(Note : xy

EGM3601SolidMechanics
Energy Methods
Chapter 14
Mechanical and Aerospace
Engineering
EquationsforAxialLoad
Normal stress
P
A
The relative displacement at the end of an axially loaded member relative to the
other end is determined from
L
P ( x )dx
A( x

EGM3601SolidMechanics
Deflection of Beams
Chapter 9
Mechanical and Aerospace
Engineering
Contents
Deformation Under Transverse
Loading
Sample Problem 9.8
Equation of the Elastic Curve
Cantilever Beams and Beams wi
th Symmetric Loadings
Bending-Moment Diag

EGM 3601 Solid Mechanics
Lecture 06: Torsion
(part 1)
Dr. Yuanli Bai, Assistant Professor
Department of Mechanical, Materials and Aerospace Engineering
University of Central Florida
Spring, 2011
EGM 3601 Solid Mechanics
1
Recall: Axial loading members
Ela

Updates
You can come by my office to pickup graded homework and exam 1.
Please write down your name on the homework when you turn it in.
EGM 3601 Solid Mechanics
1
EGM 3601 Solid Mechanics
Lecture 08: Bending
(part 3)
Dr. Yuanli Bai, Assistant Professor
D

X. Introduction to 3-D Dynamicsof
Rigid Bodies
Prof. F. Moslehy
Prof. F. Moslehy
Flywheel
A flywheel is a rotating mass which is used as an energy reservoir in a machine.
The kinetic energy is
E=
If the speed of the machine is increased, energy is stored

Jerry McMillan
Je612645
11/18/14
Pre-lab 8
Bode Plot
With PI control, the conditions completely are not satisfied completely. With PI controls, requirements
would also not be satisfied on the PM and crossover frequency.
A lag network can alter the frequen

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EGN 3343 Test 3 NAME- _ _ _ F1 _
OPEN TEXTBOOK ONLY SHOW YOUR WORK "
. Isentropic compression fr
Constant volume heat addition with a pressure ratio 0
Isentropic expansion
Constant volume heat transfer to the initial pressure
Constant pressure heat reject

EGN 3343 Test 2 NAME
OPEN TEXTBOOK ONLY SHOW YOUR WORK
Steam enters an adiabatic turbine at 1 MPa, 500C and exits at 10 kPa. During this
process, entropy is generated at 0.2 kJikg-K.
Determine the turbine eicien g.
A piston cylinder holds air at 80F and 1

EGM3601SolidMechanics
Geometric Properties of
Cross Sections
Mechanical and Aerospace
Engineering
EGM3601SolidMechanics
Objectives
Discuss the several common types of
beam shapes.
Demonstrate selected geometric
properties of cross sections applicable
to

Real Life
Examples in
Mechanics of
Solids
Lesson plans and solutions
Eann A Patterson, Editor
Real Life Examples in Mechanics of Solids
Lesson plans and solutions
First edition produced September 2006
Second Edition, 2008
Third [Electronic] Edition, 2011