MIDTERM

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1
is a branch of
mechanics that studies the internal effects of
stress and strain in a solid body that is
subjected to an external loading
Mechanics of materials
2
longitudinal stress/circumferential formula
sigma= PD/2t
3
lb/in^2 convert to lb/ft^2
lb/in^2 (12in/1ft)^2
4
N-kN
1-0.001
5
psi-ksi
1psi-0.001 ksi
6
is associated with the strength of the
material from which the body is made, while
Stress
7
is a measure of the deformation of the
body.
strain
8
performed experiments to
study the effects of loads on rods and beams
GALILEO
9
A body is subjected
to only two types of external loads;
namely surface forces AND body
forces.
EQUILIBRIUM OF DEFORMABLE BODY
10
are caused by the
direct contact of one body with
the surface of another.
Surface forces
11
is developed when one
body exerts a force on
another body without direct physical
contact between the bodies.
Body Forces
12
The surface forces that develop
at the supports or points of
contact between bodies are
reactions.
13
Equilibrium of a body requires
both these, to prevent the
body from translating or having
accelerated motion along a straight or
curved path
a balance of forces
14
this is required to prevent the body from rotating
balance of moments
15
Four types of resultant loadings:
1.Normal Force, N
2.Shear Force, V
3.Torsional moment or Torque, T
4.Bending Moment, M
16
This force acts perpendicular to the area.
Normal Force,
17
tend to cause the two
segments of the body to slide
over one another.
shear force
18
This effect is developed when
the external loads tend to twist
one segment of the body with
respect to the other about an
axis perpendicular to the area.
Torsional moment or Torque, T
19
caused by the external
loads that tend to bend the
body about an axis lying
within the plane of the area.
Bending Moment, M
20
includes the study of the body’s stability when a body
is subjected to compressive loading.
mechanics of materials
21
This subject expanded into other areas of
mechanics, such as the
theory of elasticity and the theory of plasticity.
22
which is applied to a
point on the body
concentrated force
23
if the surface loading is
applied along narrow strip of area.
linear distributed load
24
is equivalent
to the area under the distributed loading
curve, and this resultant acts through the
centroid C or geometric center of this area
resultant force
25
Procedure for Analysis
1. determine the
reactions acting on the chosen segment.
2. Draw a free-body diagram of one of the “cut”
segments and indicate the unknown resultants N, V,
M , and T at the section.
3. Equations of Equilibrium.
26
stress represents a force per unit area,
in the International Standard or SI system, the
magnitudes of both normal and shear stress are
specified in the basic units of
newtons per square
meter (N>m2 ).
27
Foot-Pound-Second system of
units, engineers usually express stress in
pounds per
square inch (psi) or kilopounds per square inch
28
where 1 kilopound (kip) = lb?
1000 lb.
29
will occur to members that are axially loaded. applied force is perpendicular
to the resisting area.
Normal stress
30
Two types of Normal Stress
Compressive stress
Tensile stress
31
Forces parallel to the area resisting the force cause shearing stress.
SHEAR STRESS
32
is the contact pressure between the separate bodies. It differs from
compressive stress, as it is an internal stress caused by compressive forces.
BEARING STRESS
33
A tank or pipe carrying a fluid or gas under a pressure is subjected to tensile
forces, which resist bursting, developed across longitudinal and transverse
sections.
THIN-WALLED VESSEL
34
Also known as unit deformation, is the ratio of the change in
length caused by the applied force,
to the original length.
Simple Stra in
35
From the origin O to the point called
p ro p o rtio n a l lim it, th e s tre s s- s tra in
c u rve is a s tra ig h t lin e . Th is lin e a r
re la tio n b e twe e n e lo n g a tio n a n d th e
a xia l fo rc e c a u s in g wa s firs t n o tic e d
b y
Sir Ro b e rt Ho o ke in 16 78
36
fo r s m a ll d e fo rm a tio n s , th e
s tre s s a n d s tra in a re p ro p o rtio n a l to e a c h o th e r,
a n d th is is kn o wn a s
Ho o ke ’s La w.
37
formula for Hooke’s Law?
F = –kx
38
is the limit beyond
wh ic h th e m a te ria l will n o lo n g e r g o
b a c k to its o rig in a l s h a p e wh e n th e
lo a d is re m o ve d , o r it is th e m a xim u m
s tre s s
elastic limit
39
s tra in d ia g ra m fro m O to E
e la s tic ra n g e
40
Th e re g io n

fro m E to R is c a lle d
p la s tic ra n g e .
41
is the point at which
th e m a te ria l will h a ve a n

a p p re c ia b le e lo n g a tio n o r

yie ld in g with o u t a n y in c re a s e in

lo a d .
Yield point
42
The maximum ordinate in the

stre ss- s tra in d ia g ra m
u ltim a te

s tre n g th o r te n s ile s tre n g th
43
the
s tre n g th o f th e m a te ria l
a t ru p tu re . Th is is a ls o
kn o wn a s th e b re a kin g

stre ng th.
Rapture strength
44
is the work done on a
u n it vo lu m e o f m a te ria l a s th e fo rc e is

g ra d u a lly in c re a s e d fro m O to P, in N·m / m 3.
Modulus of resilience
45
is the work done
o n a u n it vo lu m e o f m a te ria l a s th e fo rc e

is g ra d u a lly in c re a s e d fro m O to R, in
N·m / m 3.
Modulus of toughness
46
A body is subjected to only two types of external loads; namely,
surface forces and body
forces,
47
What are the various types of strain?
Longitudinal Strain
Volumetric Strain
Shear Strain
48
is the ratio of the steady force acting
o n a n e la s tic b o d y to th e re s u ltin g
d is p la c e m e n t. It h a s th e u n it o f N/ m m .
Stiffness
49
is a measure of the amount
o f la te ra l s tra in c a u s e d d u e to th e
lo n g itu d in a l s tra in o f m a te ria l.
Poisson's Ratio
50
is one
ha ving re la tive ly la rg e te nsile stra ins up
to th e p o in t o f ru p tu re like s tru c tu ra l
ste e l a nd a lum inum , whe re a s b rittle
m a te ria ls ha s a re la tive ly sm a ll stra in
u p to th e p o in t o f ru p tu re like c a s t iro n
a n d c o n c re t e .
d uc tile m a te ria l
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