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Co
pyri
gh
t R
. J
an
ow
–S
pri
ng
2012
Physics 111 Lecture 12
Static Equilibrium
SJ 8th Ed.: Chap 12.1 –
12.3
•Overview -Equilibrium Defined
•Conditions for Equilibrium
•Center of Gravity
–Defined
–Finding it
–When do m
ass center and CG not coincide?
•Static Equilibrium Examples
12
.1 T
he
Rig
id O
bje
ct
in E
qu
ilib
riu
m:
Th
e C
on
dit
ion
s f
or
Eq
uil
ibri
um
12
.2 M
ore
on
th
e C
en
ter
of
Gra
vit
y
12
.3 E
xam
ple
s o
f R
igid
Ob
jec
ts i
n
Sta
tic
Eq
uil
ibri
um
12
.4 E
las
tic
Pro
pe
rtie
s o
f S
oli
ds
(M
od
uli
)
Co
pyri
gh
t R
. J
an
ow
–S
pri
ng
2012
The Equilibrium Conditions
•N
o n
ew
ph
ysic
s h
ere
…ap
ply
New
ton
’s s
eco
nd
law
•
Sp
ecia
l case o
f 2
nd
Law
wit
h a
ccele
rati
on
s e
qu
al to
zero
•S
o…
net
forc
es a
nd
to
rqu
es a
re z
ero
as w
ell
{ {{{} }}}
ne
t,e
xt
L =
co
ns
tan
t
IF
.E
Q.
0 T
HE
N
=
0
se
co
nd
co
nd
itio
n m
et
τα
τα
τα
τα
r rrr
r rrr
dtL
dn
et
ext
,iα αααΙ ΙΙΙ
= ==== ===
τ τττ≡ ≡≡≡
τ τττ∑ ∑∑∑
rr
rr
Identify torques, write equations setting their sum = 0
“S
eco
nd
”co
nd
itio
n f
or
eq
uilib
riu
m0
= ===τ τττ
∑ ∑∑∑ext
,ir
{ {{{} }}}
ne
t,e
xt
p =
co
ns
tan
t
IF
F .E
Q.
0 T
HE
N
a =
0
fir
st
co
nd
itio
n m
et
r rrr r rrr
am
dtp
dF
Fn
et
ext
,i
rr
rr
= ==== ===
≡ ≡≡≡∑ ∑∑∑
Identify forces, write equations setting their sum = 0
“F
irst”
co
nd
itio
n f
or
eq
uilib
riu
m:
0= ===
∑ ∑∑∑e
xt
,iFr
Co
pyri
gh
t R
. J
an
ow
–S
pri
ng
2012
DYNAMIC VERSUS STATIC EQUILIBRIUM:
STABILITY OF STATIC EQUILIBRIUM
ISOLATED SYSTEM
MECHANICAL EQUILIBRIUM
No
ch
an
ge i
n t
ran
sla
tio
nal o
r ro
tati
on
al
“sta
te”
�co
nsta
nt
mo
men
tum
, z
ero
net
forc
e, c
on
sta
nt
an
gu
lar
mo
men
tum
, zero
net
torq
ue
�zero
lin
ear
accele
rati
on
of
part
icle
or
cm
of
rig
id b
od
y,
zero
an
gu
lar
accele
rati
on
of
rig
id b
od
y
�D
yn
am
ic:
Σ ΣΣΣF
= 0
an
d Σ ΣΣΣ
τ τττ=
0..
..B
UT
... p
an
d/o
r L
are
no
t =
0
�S
tati
c:
In
ad
dit
ion
, p
= 0
an
d L
= 0
�Im
ag
ine d
isp
lacin
g s
ys
tem
a s
mall
am
ou
nt:
do
es i
t re
turn
?
stable
unstable
neutral
EXAMPLES:
boo
k o
n ta
ble
stat
icne
utra
lpu
ck s
lidin
g on
ice
dyn
amic
--ce
ilin
g fa
n –
ondyn
amic
--ce
ilin
g fa
n –
off
stat
icne
utra
lca
r on
str
aigh
t ro
addyn
amic
--ca
r on
cur
veno
t equ
ilib
rium
--la
dder
lean
ing
agai
nst
wal
lst
atic
unst
able
(fr
icti
on)
stab
le (
foot
in
groo
ve)
Co
pyri
gh
t R
. J
an
ow
–S
pri
ng
2012
•T
he a
ctu
al w
eig
ht
can
be r
ep
laced
by t
he
weig
ht
of
a s
ing
le p
art
icle
at
the C
G
•A
sin
gle
no
n-g
ravit
ati
on
al
no
rmal
forc
e a
pp
lie
d a
t th
e C
G c
an
p
rod
uce t
ran
sla
tio
na
l eq
uil
ibri
um
balance a ruler see-saw a box about to tip
m
L
m1
m2 <
m1
L1
L2
•G
ravit
ati
on
al
torq
ues c
an
ce
l ab
ou
t th
e C
G
•A
sin
gle
su
pp
ort
fo
rce
at
the
CG
cre
ate
s z
ero
ad
ded
to
rqu
e (
mo
men
t arm
= 0
)…..
. an
d c
an
can
cel
the w
eig
ht
forc
es
(li
near
eq
uil
ibri
um
)
•C
G o
ften
co
inc
ides w
ith
mass c
en
ter
(CM
) ..
. b
ut
ma
y n
ot
if g
ravit
y v
ari
es a
cro
ss
th
e b
od
y
Definition: The center of gravityof a body is the point
about which all of the torquesdue to gravitational forces
alone add up to zero
Co
pyri
gh
t R
. J
an
ow
–S
pri
ng
2012
�12.1. The center of gravity for a sledge hammer lies on the
centerline of the handle, close to the head, at the X mark. Suppose
you saw across the handle through the center of gravity, cuttingthe
ax in two pieces. You then weigh both pieces. Which of the following
will you find?
Center of gravity for a sledge hammer
A)
Th
e h
an
dle
pie
ce is h
ea
vie
r th
an
th
e h
ea
d p
iec
e
B)
Th
e h
ead
pie
ce i
s h
ea
vie
r th
an
th
e h
an
dle
pie
ce
C)
Th
e t
wo
pie
ces a
re e
qu
all
y h
ea
vy
D)
Th
e c
om
para
tive w
eig
hts
dep
en
d o
n m
ore
in
form
ati
on
Definition: The center of gravityof a body
is the point about which all of the torques
due to gravitational forces sum to zero
x
Co
pyri
gh
t R
. J
an
ow
–S
pri
ng
2012
Center of gravity: Summary
•If the object has constant density
and is symmetrical, the center of
gravity coincides with its geometric
center.
•The sum of gravitational forces
acting on all the various mass
elements is equivalent to a single
gravitational force (the total
weight) acting through a single point
called the center of gravity (CG)
•The net torque due to gravitational
forces on an object of mass M
equals the force Mg acting at the
center of gravity of the object.
•If g is uniform over the object,
then the center of gravity of the
object coincides with its center of
mass.
Co
pyri
gh
t R
. J
an
ow
–S
pri
ng
2012
Example: Find the balance point (CG) for a level see-saw
To
lo
cate
CG
co
ord
ina
te “
s”
•P
ick l
ikely
CG
lo
cati
on
.
•S
et
su
m o
f to
rqu
es a
rou
nd
it
= 0
, in
clu
din
g o
nly
gra
vit
ati
on
al
forc
es
•S
up
po
rt f
orc
e N
ap
pli
ed
at
CG
exert
s z
ero
to
rqu
e,
pro
vid
es l
inear
eq
uil
ibri
um
FBD
m1
m2
L
xs
balance point = CG
Balance means: Find the CG and put a support force N (= total weight) there:
•Linear acceleration is zero (“static translational equilibrium”)
•Angular acceleration is also zero (“rotational equilibrium”)s
L -
sm
1g
m2g
N
If a
n o
bje
ct
is in
eq
uilib
riu
m, th
en
th
e n
et
torq
ue =
0 f
or
an
y a
xis
ch
osen
(m
ore
belo
w).
•
Fo
r an
axis
no
t at
the C
G, to
rqu
e d
ue t
o N
is n
ot
zero
bu
t sti
ll c
an
cels
th
e g
ravit
ati
on
al to
rqu
es
gm
gm
N
a)m
m(
F
y2
12
10
0− −−−
− −−−= ===
= ===+ +++
⇒ ⇒⇒⇒= ===
∑ ∑∑∑ w
eig
ht
tota
l
g )
m m(
N
2
1+ +++
= ===∴ ∴∴∴
2)
1)
0
N
)s
L(g
m
g
sm
x
cg
+ +++− −−−
− −−−⇒ ⇒⇒⇒
= ===τ τττ
∑ ∑∑∑2
10
cg
lo
cate
s2
L )m
m(
m
s
21
+ +++= ===
∴ ∴∴∴E
x:
Let
m1
= 2
m2
then
s =
1/3
L
Co
pyri
gh
t R
. J
an
ow
–S
pri
ng
2012
Locating CG’s of rigid bodies
-Pic
k b
od
y u
p (
exte
rnal
forc
e T
) an
d le
t it
sw
ing
fre
ely
,
co
me
to e
qu
ilib
riu
m p
osit
ion
, a
nd
sto
p (
fric
tio
n).
-B
od
y c
om
es
to
rest
wit
h C
G
belo
w o
r ab
ove
su
sp
en
sio
n p
oin
t,
o/w
torq
ue w
ou
ld n
ot
= z
ero
an
d
bo
dy w
ou
ld n
ot
be in
eq
uil
ibri
um
.
-M
ark
a v
ert
ical
lin
e a
t s
usp
en
sio
n p
oin
t-
Rep
eat
pro
ces
s f
or
a d
iffe
ren
t su
sp
en
sio
n p
oin
t-
Th
e C
G is
wh
ere
th
e l
ines
in
ters
ect.
T
pre
vio
us
suspensio
n
poin
t
If gravitation field is uniform, CG & CM coincide but may not beat
geometrical symmetry points unless density is uniform.
•For uniform sphere, cube, disc, rectangle,.. CG at center
•For cone. cylinder, bar, etc CG along axis of symmetry
•For composite objects, break into shapes with symmetry
WEIGHT
ACTS AT
CG
STABILITY
Block tips if CG is to the left of
all support points in base.
Net torque then can not = 0
W
N
Co
pyri
gh
t R
. J
an
ow
–S
pri
ng
2012
For Equilibrium Problems: Does it matter w
hich rotation axis you
choose for calculating torques? No. Choose any convenient axis.
O'
ro
O
axes
an
yab
ou
t
sam
e
the
is
net
i
he
nt
0
F
If
τ τττ
= ===∴ ∴∴∴
∑ ∑∑∑v
v
Not
e al
so: if
Pcm
= 0
, th
e an
gula
r m
oment
um is
the
sam
e a
roun
d a
ll p
aral
lel ax
es
O
ax
isa
bo
ut
m
om
en
tum
a
ng
ula
ri
iO
pr
L
vv
r× ×××
= ===∑ ∑∑∑
Compare rotation axis at O with one shifted to O’
for a system of point particles { mi}
ori
gin
O
'
to
by
axis
sh
ift
ii
a
a
'
r
rr
rr
r+ +++
= ===
ii
' ii
' iO
p
a
pr
p ]
a r[
L
vr
vv
vr
vr
∑ ∑∑∑∑ ∑∑∑
∑ ∑∑∑× ×××
+ +++× ×××
= ===× ×××
+ +++= ===
�Take the time derivative of each term, use second law (rotational and linear)
angular momentum
relative to axis O
angular momentum
relative to axis O’
linear momentum
of mass center
cm
P
v≡ ≡≡≡
o'
L
r
= ===
dt
Pd
a
d
t
Ld
dtL
dcm
'O
O
rr
rr
× ×××+ +++
= ===
o'
n
et,
τ τττ= ===
vo
net,
τ τττ= ===
vext
n
et,
F
r
= ===
Rightmost term vanishes
if F
net= Σ ΣΣΣFi= 0
O
O’
irv
i'rv
av
Proof:
mi
IF F
net=
0 T
HE
N τ τττ
netis
th
e s
am
e a
rou
nd
eve
ry p
ara
lle
l ax
is ..s
o...
IFτ τττ n
et=
0 f
or
on
e a
xis
TH
EN
it
is z
ero
fo
r e
ve
ry o
the
r a
xis
Co
pyri
gh
t R
. J
an
ow
–S
pri
ng
2012
Rules for solving equilibrium problems
Fir
st
Co
nd
itio
n:
Seco
nd
Co
nd
itio
n:
0= ===
ne
tFr
0= ===
τ τττn
et
r
For plane statics (flat world)
�All forces lie in x-y plane. F
z always equals zero
�All torques lie along +/-
z axis. τ τττx,
τ τττ y= 0
00
= ==== ===
= ==== ===
∑ ∑∑∑∑ ∑∑∑
y,iy,
net
x,ix,
net
FF
,F
F
0= ===
τ τττ= ===
τ τττ∑ ∑∑∑
z,iz,
ne
t
Ch
oo
se
an
y c
on
ve
nie
nt
ax
is f
or
torq
ue
ca
lcu
lati
on
.F
irst
co
nd
itio
n im
plie
s t
ha
t re
su
lt w
ill b
e t
he
sam
e (
se
e p
roo
f)fo
r a
ny r
ota
tio
n a
xis
Ca
lcu
late
to
rqu
es
du
e t
o w
eig
ht
of
rig
id b
od
ies
by p
lac
ing
th
eir
w
eig
hts
at
the
ir c
en
ter
of
gra
vit
y l
oc
ati
on
s (
see
pro
of)
Us
e s
tati
c f
ric
tio
n f
orc
e w
here
ne
ed
ed
:N
fs
sµ µµµ
≤ ≤≤≤
Co
pyri
gh
t R
. J
an
ow
–S
pri
ng
2012
�12.2. The figure shows five sketches of a uniform rod with two
or more forces acting perpendicular to it. The magnitudes of
the forces can be adjusted to any value needed, except zero.
For which of the sketches can the rod be in translational
equilibrium?
When can a system be in equilibrium?
A)
1, 2
,3 ,
4 ,
5
B
) 4
C)
2,
3, 4,
5
D
) 3
, 4
, 5
E)
4, 5
1 2 3
4 5
�12.3. For which of the situations can the rod be in overall
static equilibrium?
Net torque is the same for any
convenient axis when net force = 0
Co
pyri
gh
t R
. J
an
ow
–S
pri
ng
2012
Method for Solving Equilibrium Problems
ESSENTIALLY THE SAME AS FOR SOLVING SECOND LAW PROBLEMS
�D
raw
ske
tch, la
bel it
, deci
de w
hat
is
in o
r ou
t of
the “
syst
em
”.�
Dra
w f
ree b
ody
dia
gram
s.
Inc
lude f
orce
s O
Nth
e b
ody
bein
g an
alyz
ed. S
how
poi
nt o
f ap
plic
atio
n to
ind
icat
e t
orqu
es.
�C
hoo
se a
xes
and t
he +
/-se
nse f
or r
otat
ions
. R
epl
ace f
orce
s by
their
x, y,
z c
ompo
nent
s
00
0= ===
τ τττ= ===
= ===∑ ∑∑∑
∑ ∑∑∑∑ ∑∑∑
zy
x
,F
,F
�C
hoo
se a
rot
atio
n ax
is/p
oint
to
use in
calc
ulat
ing
torq
ues.
oA
ll c
hoi
ces
yield
the s
ame n
et
torq
ue, so
lon
g as
the F
irst
equ
ilib
rium
con
dit
ion
appl
ies…
but
...o
Som
e c
hoi
ces
sim
plif
y th
e s
olut
ion.
Loo
k f
or w
ays
to g
ive z
ero
mom
ent
arm
(zero
tor
que)
to irr
ele
vant
or
trou
ble
som
e f
orce
s.�
App
ly
(2 d
imens
ions
)�
Sub
stit
ute t
he a
ctua
lfor
ces
and t
orqu
es
into
the e
quat
ions
.�
Cou
nt t
he u
nkno
wns
; m
ake s
ure t
here
are
N e
quat
ions
when
there
are
N u
nkno
wns
. C
onst
rain
t equ
atio
ns a
re o
ften
needed.
�S
olve
the s
et o
f “s
imul
tane
ous
equ
atio
ns”
alge
bra
ical
ly a
s fa
ras
is
reas
onab
le b
efo
re s
ubst
itut
ing
num
bers
.�
Try
to
inte
rpre
t re
sult
ing
equa
tion
s in
tuit
ively
. C
heck
that
nu
meri
cal an
swers
mak
e s
ens
e, hav
e r
eas
onab
le m
agni
tudes,
phys
ical
uni
ts, etc
.
Co
pyri
gh
t R
. J
an
ow
–S
pri
ng
2012
Example: Mechanical Advantage of a pulley system
Th
e p
ulle
y s
ys
tem
is u
se
d t
o r
ais
e a
weig
ht
slo
wly
at
co
nsta
nt
sp
eed
( a
= 0
).
Use t
he
eq
uil
ibri
um
co
nd
itio
ns a
nd
fre
e b
od
y
dia
gra
ms t
o f
ind
th
e t
en
sio
n in
each
cab
le
an
d t
he l
ifti
ng
fo
rce.
Th
e p
ulle
ys
are
massle
ss
an
d f
ricti
on
less.
Solution requires “first condition”
only
�At each pulley, the sum of upward =
the sum of downward forces
TA
TA
TB
TB
= 2
TA
W =
98
00 N
T1
T2
T2
T3
T3
T3
T4
N
9800
W
T
= ==== ===
∴ ∴∴∴1
N
4900
T
T
T2
21
= ===⇒ ⇒⇒⇒
= ===2
N
2450
T
T
T
23
2= ===
⇒ ⇒⇒⇒= ===
3
N
49
00
T
2T
T4
3= ===
⇒ ⇒⇒⇒= ===
4
Mechanical advantage
(weight lifted/force exerted)
4
2450
9800
TW= ===
= ===3
Co
pyri
gh
t R
. J
an
ow
–S
pri
ng
2012
Example: Angle of the chair lift cable
Th
e c
ha
ir l
ift
is a
t th
e m
idd
le o
f t
he c
ab
le
sp
an
as s
ho
wn
. I
t’s w
eig
ht
cau
ses t
he
cab
le
to d
efl
ec
t b
y a
n a
ng
le θ θθθ
fro
m t
he h
ori
zo
nta
l o
n
bo
th s
ides o
f th
e c
hair
. T
he
pu
lle
ys
are
mass
-
less a
nd
fri
cti
on
less.
Th
e s
kie
r w
eig
hs 7
8 k
g.
Fin
d t
he a
ng
le θ θθθ
wh
en
th
e h
an
gin
g w
eig
ht
is
2200 N
as
sh
ow
n.
m =
78 k
g
W =
2200 N
θ θθθ
T is u
nif
orm
an
d T
= 2
200 N
TT
mg
θ θθθθ θθθ
Fre
e b
od
y d
iag
ram
mg
)
sin
(T
F
y− −−−
θ θθθ= ===
= ===∑ ∑∑∑
20
17
37
02
20
02
89
78
2.
x
.
x
T
mg
)sin
(= ===
= ==== ===
θ θθθ
.
o0
10
= ===θ θθθ
Co
pyri
gh
t R
. J
an
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–S
pri
ng
2012
PP
10603-0
8:
A c
ar
wh
ose m
ass =
1360 k
g h
as 3
.05 m
betw
een
its
fro
nt
an
d r
ear
axle
s. It
s c
en
ter
of
gra
vit
y i
s lo
cate
d 1
.78 m
beh
ind
th
e f
ron
t axle
. T
he c
ar
is s
tati
on
ary
on
level g
rou
nd
. F
ind
th
e
mag
nit
ud
e o
f th
e f
orc
e f
rom
th
e g
rou
nd
on
each
fro
nt
an
d r
ear
wh
eel (a
ssu
min
g e
qu
al fo
rces o
n
bo
th s
ides o
f th
e c
ar)
.
Example: Distributing weight between front and rear wheels of a car
2F
R2F
F
L=
3.0
5 m
mg
d =
1.7
8 m
Solution: apply “first”and “second”equilibrium
conditions. Calculate torques using axis
through rear wheel contact point with the
ground. m
g =
1360 k
g x
9.8
= 1
3,3
28 N
.
0
F
x= ===
∑ ∑∑∑m
g
F
2 F
2
F
FR
y− −−−
+ +++= ===
= ===∑ ∑∑∑
0
FR
an
d F
Fare
fo
rces o
n e
ac
h w
heel
L
2F
d)
-m
g(L
F 2
x
Fx
Ro
+ +++− −−−
= ==== ===
τ τττ∑ ∑∑∑
00
To
rqu
es a
bo
ut
rear
wh
eels
3.0
5
x 2
1.7
8)
- (3
.05
x
13
,32
8
L2
d)
-m
g(L
F
F= ===
= ===
2
55
50
- 1
3,3
28
2
2F
- m
g
F
FR
= ==== ===
N.
2
77
5
F
F= ===
N.
3
88
9
F R
= ===
Co
pyri
gh
t R
. J
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–S
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2012
Example: A meter stick balances horizontally on a knife-edge at the 50.0
cm mark. When two 5.0 g coins are attached over the 12.0 cm mark
the
stick now balances at the 45.5 cm mark. What is the mass of the meter
stick?
Problem PP10603-11:
m =
2 x
5 g
m =
.01 k
gx
1=
0.1
2 m
x2
=
.455 m
X3
= 0
.5 m
M
= m
ete
r s
tick
mass
0 c
m10
0 c
m
x1
mg
Mg
Nx
2
x3
APPLY EQUILIBRIUM CONDITIONS:
Mg
mg
N
F
y− −−−
− −−−= ===
= ===∑ ∑∑∑
0
Mg
mg
N + +++
= ===
•M
ete
r sti
ck a
lon
e a
cts
lik
e a
mass M
co
ncen
trate
d a
t it
s o
wn
CG
at
x3
= 0
.5 m
•C
ho
ose a
xis
fo
r to
rqu
es a
t 0 c
m (
left
en
d o
f sti
ck).
A
ny o
ther
axis
yie
lds s
am
e n
et
torq
ue
g
xM
Nx
mg
x-
32
1o
− −−−+ +++
= ==== ===
τ τττ∑ ∑∑∑
0
g
xM
Mg
xm
gx
mg
x-
32
1− −−−
+ ++++ +++
= ===2
0
]x
x [M
]x -
xm
[
3
12
− −−−+ +++
= ===2
0
2
3
10
44
74
55
50
0
12
45
50
10
− −−−= ===
− −−−− −−−= ===
− −−−= ===
x.
..
..
. ]
xx [
]x -
xm
[
M
2
12
g
m
.
M
47
4= ===
Co
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gh
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2012
�12.4. The sketches show four overhead views of uniform disks that
can slide or rotate on a frictionless floor. Three forces act on each
disk, either at the rim or at the center. The force vectors rotate
along with the disks, so the force arrangements remain the same.
Which disks are in equilibrium?
Find the forces on the pivot
A)
1, 2, 3, 4
B)
1, 3, 4
C)
3D
)1, 4
E)
3, 4
F
2F
3F
1
FF
2F
2
FF
2F
3
F
2F
4 F
0= ===
net
Fr0
= ===τ τττ
ne
t
r
Co
pyri
gh
t R
. J
an
ow
–S
pri
ng
2012
Example 1: Massless
beam supporting a weight
Th
e 2
.4 m
. lo
ng
weig
htl
ess b
eam
sh
ow
n in
th
e f
igu
re is
su
pp
ort
ed
on
th
e r
igh
t b
y a
cab
le t
hat
makes a
n a
ng
le o
f 5
0o
wit
h t
he h
ori
zo
nta
l b
eam
. A
32 k
g m
ass h
an
gs f
rom
th
e b
eam
1.5
m f
rom
th
e p
ivo
t p
oin
t o
n t
he left
.
a)
Calc
ula
te t
he t
orq
ue c
au
sed
by t
he h
an
gin
g m
ass.
b)
Dete
rmin
e t
he c
ab
le t
en
sio
n t
hat
pro
du
ces e
qu
ilib
riu
m
Choose: rotation axis at O o
T
θ θθθ
mg
Fx
Fy
x
Draw FBD of beam
Part a)
m.N
.
x .
x
mg
x
mass
470
51
89
32
− −−−= ===
− −−−= ===
− −−−= ===
τ τττ
m 2.4
L
m,
1.5
x
,o
= ==== ===
= ===θ θθθ
50
Part b)
meq
uil
ibri
u
for
o
0= ===
τ τττ∑ ∑∑∑
)T
sin
(
T
T
LT
m
gx
-
b
ea
m
to
o
fc
om
po
ne
nt
y
y
θ θθθ= ===
= ===
+ +++= ===
⊥ ⊥⊥⊥
0
N
.
)L
sin
(
mg
x
T
25
6= ===
θ θθθ= ===
m =
32 k
g
x
O
Co
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t R
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2012
For the preceding problem, find the x component of the force at the
pivot point. What equations can you use?
Example 1, continued: Find the forces on the pivot
Fir
st
Co
nd
itio
n:
Seco
nd
Co
nd
itio
n:
0= ===
ne
tFr
0= ===
τ τττn
et
r
o
T
θ θθθ
mg
Fx
Fy
x
m 2.4
L
m,
1.5
x
,o
= ==== ===
= ===θ θθθ
50
N
.
)L
sin
(
mg
x
T
256
= ===θ θθθ
= ===
For the preceding problem, find the y component of the force at the
pivot point. What equations can you use?
F
-T
0
F
xx
x= ===
= ===∑ ∑∑∑
N 1
65
)
Tc
os
(F
x
= ===θ θθθ
= ===
)T
sin
(
m
g -
F
0
F
y
yθ θθθ
+ +++= ===
= ===∑ ∑∑∑
N 1
17
)
Ts
in(
mg
-
F
y
= ===θ θθθ
− −−−= ===
Co
pyri
gh
t R
. J
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–S
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2012
Example 2: As in previous problem but beam has mass now
Th
e 2
.4 m
. lo
ng
beam
sh
ow
n in
th
e f
igu
re is s
up
po
rted
on
th
e r
igh
t b
y a
cab
le t
hat
makes a
n a
ng
le o
f 5
0o
wit
h t
he h
ori
zo
nta
l b
eam
. A
32 k
g m
ass h
an
gs f
rom
th
e b
eam
1.5
m f
rom
th
e p
ivo
t p
oin
t o
n t
he
left
.
a)
Dete
rmin
e t
he c
ab
le t
en
sio
n n
eed
ed
to
pro
du
ce e
qu
ilib
riu
mb
)F
ind
th
e f
orc
es a
t p
oin
t “O
”
MB= mass of beam = 30 kg acts as point mass
at CG of beam.
Choose: rotation axis at O
m =
32 k
g
x
O
o
T
θ θθθ
mg
Fx
Fy
x
MBg
L/2
FBD of beam
L/2
at
C
G
m,
2
.4L
m,
1
.5x
,o
= ==== ===
= ===θ θθθ
50
meq
uil
ibri
u
for
o
0= ===
τ τττ∑ ∑∑∑
)T
sin
(
T
T
L
T g
M
mg
x -
be
am
to
of
co
mp
on
en
t y
y2L
B
θ θθθ= ===
= ===
+ +++− −−−
= ===
⊥ ⊥⊥⊥
0
N
.
)L
sin
(
gM
mg
x
T
LB
44
82
= ===θ θθθ
+ +++= ===
Part a)
Part b)
)co
s(
TF
F
xx
θ θθθ− −−−
= ==== ===
∑ ∑∑∑0
N.
)
co
s(
TF
x2
88
= ===θ θθθ
= ===
gM
mg
)sin
(T
F
FB
yy
− −−−− −−−
θ θθθ+ +++
= ==== ===
∑ ∑∑∑0
N
.
264
)
sin
(T
gM
mg
F B
y= ===
θ θθθ− −−−
+ +++= ===
Co
pyri
gh
t R
. J
an
ow
–S
pri
ng
2012
Example 3:
A u
nif
orm
beam
, o
f le
ng
th L
an
d m
ass m
= 1
.8 k
g, is
at
rest
wit
h i
ts e
nd
s
on
tw
o s
cale
s (
see f
igu
re).
A
un
ifo
rm b
lock, w
ith
mass M
= 2
.7 k
g,
is a
t re
st
on
th
e b
eam
, w
ith
its
cen
ter
a d
ista
nce L
/ 4
fro
m t
he b
eam
's l
eft
en
d.
What do the scales read?
Solve as equilibrium system
Axis at “o”is convenient
Beam weight acts as if it is at
CG of beam (x = L/2)
o
FB
D
Co
pyri
gh
t R
. J
an
ow
–S
pri
ng
2012
Example 3: Solution
2:
1:
3:Scale readings are normal forces and
L Fr
R Fr
mg
F
M
g
Fb
eam
g,
blo
ck
,g
= ==== ===
imp
act
n
ox
0
F
= ===∑ ∑∑∑
mg
Mg
F
F
0
FR
Ly
− −−−− −−−
+ +++= ===
= ===∑ ∑∑∑ Choose axis for torques at left of beam L
F
2L
mg
-
4LM
g -
0
F
0
R
x
L+ +++
= ==== ===
τ τττ∑ ∑∑∑ From 2:
Solve
2
LLm
g
4
LLM
g
FR
+ +++= ===
15
.44
2
mg
4Mg
F
2
9.8
x
1.8
4
9.8
x
2.7
R= ===
= ===+ +++
= ===+ +++
N
.
15
F
R≈ ≈≈≈
mg
Mg
43
2
mg
4Mg
mg
Mg
FL
21+ +++
= ===− −−−
− −−−+ +++
= ===
N
.
29
28.6
8
F L
≈ ≈≈≈= ===
Block and beam
represented as particles
at their CMs(CGs)
Co
pyri
gh
t R
. J
an
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–S
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2012
Example 4:
A s
afe
wh
ose
ma
ss is
M=
43
0 k
g is
h
an
gin
g b
y a
ro
pe
fro
m a
bo
om
wit
h
dim
en
sio
ns
a=
1.9
m a
nd
b=
2.5
m.
Th
e b
oo
m c
on
sis
ts o
f a
hin
ge
d
be
am
an
d a
ho
rizo
nta
l ca
ble
th
at
co
nn
ec
ts t
he
be
am
to
a w
all. T
he
u
nif
orm
be
am
ha
s a
ma
ss
mo
f 8
5
kg
; th
e m
as
s o
f th
e c
ab
le a
nd
ro
pe
a
re n
eg
lig
ible
.
(a)
Wh
at
is t
he
te
ns
ion
Tc
in t
he
c
ab
le;
i. e
., w
hat
is t
he
ma
gn
itu
de
of
the
fo
rce
Tc
on
th
e b
ea
m f
rom
th
e
ho
rizo
nta
l ca
ble
?
(b)
Wh
at
is t
he
ma
gn
itu
de
of
the
fo
rce
at
the
hin
ge
?
Tr
Tc
mg
Fh
Fv
Co
pyri
gh
t R
. J
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2012
Example 4 Solution
Tr
Tc
mg
Fh
Fv
The b
eam
is
the s
yste
m t
o an
alyz
eT
he b
eam
’s w
eig
ht
acts
at
it’s
CG c
hc
hx
T
F
T
F
0
F
= ===∴ ∴∴∴
− −−−= ===
= ===∑ ∑∑∑
rv
yT
M
g
Mg
mg
F
0
F= ===
− −−−− −−−
= ==== ===
∑ ∑∑∑ Choose hinge point “O”as axis for torques
-Eliminates Fvand F
hin torque equation
2b
mg
bT
aT
0
r
co
− −−−− −−−
= ==== ===
τ τττ∑ ∑∑∑
)co
t(
ab
θ θθθ= ===
1.7
2.5
x
9.8
]
430
285
[
ab g
]M
2m[
T c
+ +++= ===
+ +++= ===
N
6093
T
c
= ===
N
6093
T
F
c
h= ===
= ===
9.8
)430
(85
M
g
m
g
F
v+ +++
= ===+ +++
= ===
N
5
04
7
F
v
= ===
N
7
91
2
]
F
F
[
|F|
1/2
2 v
2 h= ===
+ +++= ===
Co
pyri
gh
t R
. J
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2012
Problem:In the figure, force Fis applied horizontally at the axle of the wheel. The
wheel's radius is rand its mass is m.
Find the minimum force F needed to raise the wheel over a curb of height h.
Example 5: Does the wheel roll over the curb?
Calculate torques around
contact point with curb
Barrier when h > r
r -
h s
mg N
Px
Py
Wh
y s
uch
larg
e w
heels
?
Co
pyri
gh
t R
. J
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2012
Example 5: Can the wheel roll over the curb?
N
mg
F Px
Py
Geometry:
h r
h
rh)
hr(
rs
as
lo
ng
as
> >>>− −−−
= ===− −−−
− −−−= ===
22
22
Equations for equilibrium:
0= ===
− −−−+ +++
= ===∑ ∑∑∑
mg
PN
Fy
y
0= ===
− −−−= ===
∑ ∑∑∑x
xP
FF
0= ===
− −−−− −−−
− −−−= ===
τ τττ∑ ∑∑∑
)h
r(F
Ns
mg
s
As wheel is about to lift off and roll, N � ���
0
mg
P
y
= ===∴ ∴∴∴
xP
F = ===
22
hrh
mg
mg
sh
)-
F(r
− −−−
= ==== ===
h
rfo
r
mg
h)
-(r
hrh
F
> >>>
− −−−= ===
22
For r > h, F grows as r � ���
h.
F becomes infinite if r=h.
For r < h vehicle is stopped.
F cannot pull it over curb
When does F = mg? Ans: for r = 2h
Take
torques
around
here
r -
h
s
FBD of the W
heel
Problem:In the figure, force Fis applied horizontally at the axle of the wheel. The
wheel's radius is rand its mass is m.
Find the minimum force F needed to raise the wheel over a curb of height h.
Co
pyri
gh
t R
. J
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ow
–S
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2012
Example 6: Climbing a ladder
A ladder
wh
ose length
L=
12
m a
nd m
ass m
= 4
5 k
g leans a
gain
st
a f
riction
less)
wall.
It
s
top is a
t heig
ht
h=
9.3
m a
bove t
he p
avem
en
t
that
the lo
wer
end r
ests
on.
The p
avem
ent
is
not
fric
tionle
ss.
The ladder's o
wn m
ass c
ente
r
is L
/ 3
fro
m t
he lo
wer
end.
A f
irefighte
r of
mass M
= 7
2 k
g c
limbs t
he
ladd
er
until h
er
cente
r of
mass is s
= L
/ 2
from
the lo
wer
end.
Fin
d t
he m
agn
itudes o
f th
e f
orc
es o
n t
he
ladd
er
from
the w
all
an
d t
he p
avem
ent.
Fin
d h
ow
far
up t
he ladd
er
the f
irefighte
r ca
n
clim
b b
efo
re it
slip
s.
The s
tatic f
riction
coeff
icie
nt
betw
een ladd
er
and p
avem
ent
is
0.2
.a =
Lco
s(θ θθθ
)h
= L
sin
(θ θθθ)
S
θ θθθ
1.2
27
)
tan
(
.815
)
co
t(
50.8
.3
/12)
(sin
)
Lh (sin
o1-
1-
= ===θ θθθ
= ===θ θθθ
= ==== ===
= ===θ θθθ
9
Co
pyri
gh
t R
. J
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–S
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2012
Example 5 solution –Climbing a Ladder
S
Sx
Firefighter is a distance S from the base
)co
s(
s
sx
θ θθθ= ===
ba
se
at
forc
e
no
rma
lp
y
F≡ ≡≡≡
py
s
forc
e
fric
tio
n
sta
tic
px
F
Fµ µµµ
≤ ≤≤≤≡ ≡≡≡
we
igh
trs
fire
fig
hte
M
g≡ ≡≡≡
L/3
at
CG
la
dd
er
weig
ht,
sla
dd
er'
m
g≡ ≡≡≡
ho
rizo
nta
l
fr
icti
on
N
o
lad
der
o
n
wall
of
fo
rce
w
F⇒ ⇒⇒⇒
≡ ≡≡≡
mg
Mg
F
F
py
y− −−−
− −−−= ===
= ===∑ ∑∑∑
0
px
wx
F
F
F
− −−−= ===
= ===∑ ∑∑∑
0
Equilibrium conditions
F
F
px
w= ===
9.8
72)
(45
mg
Mg
F
p
y+ +++
= ===+ +++
= ===
N
1146
F
py
= ===
Choose axis for torques
at base of ladder “O”
)sin
(
LF
)co
s(
M
gs
)
(o
sc
3Lm
g
w
o
θ θθθ− −−−
θ θθθ+ +++
θ θθθ= ===
= ===τ τττ
∑ ∑∑∑0
Co
pyri
gh
t R
. J
an
ow
–S
pri
ng
2012
Ladder Example Solution, continued
Note:
1.
As s grows, so does FW= F
PX(friction) needed to stay in equilibrium.
2.
As
θ θθθ� ���0, frictional force needed becomes huge, ladder slips
)ta
n(g
LsM
mF
Wθ θθθ
+ +++= ===
3
Example:
For S = L/2 (halfway up):
Solve torque equation for F
w
)s
in(
L
)c
os
(M
gs
mg
LF
wθ θθθθ θθθ
+ +++= ===
3
F
N
40
8
).
tan
(
gM
mF
p
xo
w= ===
≈ ≈≈≈
+ +++
= ===8
50
23
Set impending motion condition:
Solve torque equation for s:
How far up the ladder can the firefighter climb before it
slips, assuming µ µµµ
s= 0.2
[ [[[] ]]]
gm
MF
F
F
s
py
sp
xw
+ +++µ µµµ
= ===µ µµµ
= ==== ===
)co
s(
3L
mg
)
sin
(
LF
)co
s(
M
gs
wθ θθθ
− −−−θ θθθ
= ===θ θθθ
3L
Mm
)ta
n(
L
Mg
g)m
M(
s
s− −−−
θ θθθ+ +++
µ µµµ= ===
312
72
45
1.2
27
12
45/7
2)
(1 .2
x
− −−−+ +++
= ===
m
2.3
.
s
≈ ≈≈≈
= ===∴ ∴∴∴
29
2
Getting halfway up
requires
µ µµµs>> 0.2
Co
pyri
gh
t R
. J
an
ow
–S
pri
ng
2012
Example 7: Rock Climber
In t
he
fig
ure
a r
ock c
lim
ber
wit
h m
ass
m=
55 k
g r
es
ts d
uri
ng
a “
ch
imn
ey c
lim
b,”
pre
ssin
g o
nly
wit
h h
er
sh
ou
lders
an
d f
ee
t ag
ain
st
the
walls o
f a f
issu
re o
f w
idth
w=
1.0
m.
Her
cen
ter
of
mass i
s a
ho
rizo
nta
l d
ista
nce d
= 0
.20 m
fro
m t
he
wall a
gain
st
wh
ich
her
sh
ou
lders
are
pre
ssed
. T
he
co
eff
icie
nt
of
sta
tic
fri
cti
on
betw
een
her
sh
oes a
nd
th
e w
all is µ µµµ
1=
1.1
, an
d
betw
een
her
sh
ou
lders
an
d t
he
wall it
is
µ µµµ2
= 0
.70.
To
res
t, t
he c
lim
ber
wan
ts t
o
min
imiz
e h
er
ho
rizo
nta
l p
ush
on
th
e
walls. T
he m
inim
um
occ
urs
wh
en
her
fee
t an
d h
er
sh
ou
lders
are
bo
th o
n t
he v
erg
e
of
sli
din
g.
(a)
Wh
at
is t
he m
inim
um
ho
rizo
nta
l p
ush
on
th
e w
all
s?
(i
mp
en
din
g m
oti
on
)
(b)
Wh
at
sh
ou
ld t
he v
ert
ical
dis
tan
ce h
be b
etw
een
th
e
sh
ou
lders
an
d f
eet,
in
ord
er
for
her
to r
em
ain
sta
tio
nary
?
µ µµµ1
µ µµµ2
Co
pyri
gh
t R
. J
an
ow
–S
pri
ng
2012
Solution of Example 7: Rock Climber
w =
1.0
m
O
Fin
d t
he m
inim
um
ho
rizo
nta
l p
ush
on
th
e w
alls.
The climber is the system to analyze
N'
N
N'
N
Fx
= ===⇒ ⇒⇒⇒
− −−−= ===
= ===∑ ∑∑∑
0
mg
f
f
F
21
y− −−−
+ +++= ===
= ===∑ ∑∑∑
0
For impending slippage:
N
f
N
f2
2µ µµµ
= ===µ µµµ
= ===1
1
mg
N )
(
21
= ===µ µµµ
+ +++µ µµµ
N
30
0
)
(
mg
N
0.7
1.1
9.8
x
55
21
= ==== ===
µ µµµ+ +++
µ µµµ= ===
+ +++
m 0.7
4
d)
dw(
N
mg
dN
wµ
h
wf
h
N
m
gd
x'N
x
f
1
o
= ===µ µµµ
− −−−− −−−
µ µµµ= ===
− −−−= ===
∴ ∴∴∴
− −−−+ +++
+ ++++ +++
= ==== ===
τ τττ∑ ∑∑∑
21
12
00
0
Th
is c
ho
ice
of
h p
rod
uces i
mp
en
din
g m
oti
on
Wh
at
sh
ou
ld t
he v
ert
ical
dis
tan
ce h
be
be
tween
sh
ou
lders
an
d f
eet?
C
ho
ose a
xis
fo
r to
rqu
es
at
po
int
“O
”