Fluid Mechanics , 6th Edition Solution Manual

Name: Fluid Mechanics , 6th Edition Solution Manual
Brand: Academic Documents Platform
Price: 17 USD
Availability: InStock
Author: Theodore Long

Fluid Mechanics, 6th Edition Solution Manual is the ultimate guide to solving textbook questions, offering easy-to-follow solutions.

Theodore Long

Contributor

4.1

4 months ago

Preview (16 of 729)

Fluid Mechanics, 6 th Ed. Kundu, Cohen, and Dowling
Exercise 1.1. Many centuries ago, a mariner poured 100 cm 3 of water into the ocean. As time
passed, the action of currents, tides, and weather mixed the liquid uniformly throughout the
earth’s oceans, lakes, and rivers. Ignoring salinity, estimate the probability that the next sip (5
ml) of water you drink will contain at least one water molecule that was dumped by the mariner.
Assess your chances of ever drinking truly pristine water. (Consider the following facts: M w for
water is 18.0 kg per kg-mole, the radius of the earth is 6370 km, the mean depth of the oceans is
approximately 3.8 km and they cover 71% of the surface of the earth.)
Solution 1.1. To get started, first list or determine the volumes involved:
υd = volume of water dumped = 100 cm 3 ,
υc = volume of a sip = 5 cm3 , and
V = volume of water in the oceans =
€
4
πR2D
γ ,
where, R is the radius of the earth, D is the mean depth of the oceans, and
γ is the oceans'
coverage fraction. Here we've ignored the ocean volume occupied by salt and have assumed that
the oceans' depth is small compared to the earth's diameter. Putting in the numbers produces:
€
V = 4
π (6.37 ×10 6 m) 2 (3.8 ×10 3 m)(0.71) = 1.376 ×1018 m3 .
For well-mixed oceans, the probability Po that any water molecule in the ocean came from the
dumped water is:
€
Po = (100 cm 3 of water)
(oceans' volume) =
υd
V = 1.0 ×10−4 m3
1.376 ×1018 m3 = 7.27 ×10−23 ,
Denote the probability that at least one molecule from the dumped water is part of your next sip
as P1 (this is the answer to the question). Without a lot of combinatorial analysis, P1 is not easy
to calculate directly. It is easier to proceed by determining the probability P2 that all the
molecules in your cup are not from the dumped water. With these definitions, P1 can be
determined from: P1 = 1 – P2 . Here, we can calculate P2 from:
P2 = (the probability that a molecule was not in the dumped water) [number of molecules in a sip] .
The number of molecules, Nc, in one sip of water is (approximately)
N c = 5cm3 × 1.00g
cm3 × gmole
18.0g × 6.023×10 23 molecules
gmole = 1.673×10 23 molecules
Thus, P2 = (1− Po )N c = (1− 7.27 ×10−23 )1.673×10 23
. Unfortunately, electronic calculators and modern
computer math programs cannot evaluate this expression, so analytical techniques are required.
First, take the natural log of both sides, i.e.
ln(P2 ) = N c ln(1− Po ) = 1.673×10 23 ln(1− 7.27 ×10−23 )
then expand the natural logarithm using ln(1–
ε) ≈ –
ε (the first term of a standard Taylor series
for
€
ε → 0)
ln(P2 ) ≅ −N c ⋅ Po = −1.673×10 23 ⋅ 7.27 ×10−23 = −12.16 ,
and exponentiate to find:
P2 ≅ e−12.16 ≅ 5×10−6 ... (!)
Therefore, P1 = 1 – P2 is very close to unity, so there is a virtual certainty that the next sip of
water you drink will have at least one molecule in it from the 100 cm3 of water dumped many
years ago. So, if one considers the rate at which they themselves and everyone else on the planet
uses water it is essentially impossible to enjoy a truly fresh sip.

Fluid Mechanics, 6 th Ed. Kundu, Cohen, and Dowling
Exercise 1.2. An adult human expels approximately 500 ml of air with each breath during
ordinary breathing. Imagining that two people exchanged greetings (one breath each) many
centuries ago, and that their breath subsequently has been mixed uniformly throughout the
atmosphere, estimate the probability that the next breath you take will contain at least one air
molecule from that age-old verbal exchange. Assess your chances of ever getting a truly fresh
breath of air. For this problem, assume that air is composed of identical molecules having M w =
29.0 kg per kg-mole and that the average atmospheric pressure on the surface of the earth is 100
kPa. Use 6370 km for the radius of the earth and 1.20 kg/m 3 for the density of air at room
temperature and pressure.
Solution 1.2. To get started, first determine the masses involved.
m = mass of air in one breath = density x volume =
€
1.20kg /m3
( ) 0.5 ×10−3 m3
( ) =
€
0.60 ×10−3 kg
M = mass of air in the atmosphere =
€
4
πR2
ρ(z)dz
z= 0
∞
∫
Here, R is the radius of the earth, z is the elevation above the surface of the earth, and
ρ(z) is the
air density as function of elevation. From the law for static pressure in a gravitational field,
€
dP dz = −
ρg, the surface pressure, Ps, on the earth is determined from
€
Ps − P∞ =
ρ(z)gdz
z= 0
z= +∞
∫ so
that: M = 4
π R2 Ps − P∞
g = 4
π (6.37 ×10 6 m) 2 (10 5 Pa)
9.81ms−2 = 5.2 ×1018 kg .
where the pressure (vacuum) in outer space = P∞ = 0, and g is assumed constant throughout the
atmosphere. For a well-mixed atmosphere, the probability Po that any molecule in the
atmosphere came from the age-old verbal exchange is
€
Po = 2 × (mass of one breath)
(mass of the whole atmosphere) = 2m
M = 1.2 ×10−3 kg
5.2 ×1018 kg = 2.31×10−22 ,
where the factor of two comes from one breath for each person. Denote the probability that at
least one molecule from the age-old verbal exchange is part of your next breath as P1 (this is the
answer to the question). Without a lot of combinatorial analysis, P1 is not easy to calculate
directly. It is easier to proceed by determining the probability P2 that all the molecules in your
next breath are not from the age-old verbal exchange. With these definitions, P1 can be
determined from: P1 = 1 – P2 . Here, we can calculate P2 from:
P2 = (the probability that a molecule was not in the verbal exchange) [number of molecules in one breath] .
The number of molecules, Nb, involved in one breath is
€
N b = 0.6 ×10−3 kg
29.0g /gmole × 10 3 g
kg × 6.023 ×10 23 molecules
gmole = 1.25 ×10 22 molecules
Thus,
€
P2 = (1− Po )N b = (1− 2.31×10−22 )1.25×10 22
. Unfortunately, electronic calculators and modern
computer math programs cannot evaluate this expression, so analytical techniques are required.
First, take the natural log of both sides, i.e.
€
ln(P2 ) = N b ln(1− Po ) = 1.25 ×10 22 ln(1− 2.31×10−22 )
then expand the natural logarithm using ln(1–
ε) ≈ –
ε (the first term of a standard Taylor series
for
€
ε → 0)
€
ln(P2 ) ≅ −N b ⋅ Po = −1.25 ×10 22 ⋅ 2.31×10−22 = −2.89,
and exponentiate to find:

Fluid Mechanics, 6 th Ed. Kundu, Cohen, and Dowling
Exercise 1.3. The Maxwell probability distribution, f(v) = f(v1 ,v2 ,v3 ), of molecular velocities in a
gas flow at a point in space with average velocity u is given by (1.1).
a) Verify that u is the average molecular velocity, and determine the standard deviations (
σ1 ,
σ2 ,
σ3 ) of each component of u using
σ i = 1
n (vi − ui ) 2
all v
∫∫∫ f (v)d3v
#
$
% &
'
(
1 2
for i = 1, 2, and 3.
b) Using (1.27) or (1.28), determine n = N/V at room temperature T = 295 K and atmospheric
pressure p = 101.3 kPa.
c) Determine N = nV = number of molecules in volumes V = (10 μm) 3 , 1 μm3 , and (0.1 μm) 3 .
d) For the ith velocity component, the standard deviation of the average,
σa,i, over N molecules
is
σa,i =
σ i N when N >> 1. For an airflow at u = (1.0 ms–1 , 0, 0), compute the relative
uncertainty, 2
σ a,1 u1 , at the 95% confidence level for the average velocity for the three volumes
listed in part c).
e) For the conditions specified in parts b) and d), what is the smallest volume of gas that ensures
a relative uncertainty in U of one percent or less?
Solution 1.3. a) Use the given distribution, and the definition of an average:
(v)ave = 1
n v
all u
∫∫∫ f (v)d3v = m
2
π k B T
"
#
$ %
&
'
3 2
v
−∞
+∞
∫
−∞
+∞
∫
−∞
+∞
∫ exp − m
2k B T v − u 2*
+
,
-
.
/ d3v .
Consider the first component of v, and separate out the integrations in the "2" and "3" directions.
(v1 )ave = m
2
π k B T
!
"
# $
%
&
3 2
v1
−∞
+∞
∫
−∞
+∞
∫
−∞
+∞
∫ exp − m
2k B T (v1 − u1 ) 2 + (v2 − u2 ) 2 + (v3 − u3 ) 2*+ ,-
.
/
0
1
2
3 dv1dv2dv3
= m
2
π k B T
!
"
# $
%
&
3 2
v1
−∞
+∞
∫ exp − m(v1 − u1 ) 2
2k B T
*
+
,
-
.
/ dv1 exp − m(v2 − u2 ) 2
2k B T
*
+
,
-
.
/ dv2
−∞
+∞
∫ exp − m(v3 − u3 ) 2
2k B T
*
+
,
-
.
/−∞
+∞
∫ dv3
The integrations in the "2" and "3" directions are equal to:
€
2
πk B T m( )1 2
, so
(v1 )ave = m
2
π k B T
!
"
# $
%
&
1 2
v1
−∞
+∞
∫ exp − m(v1 − u1 ) 2
2k B T
*
+
,
-
.
/ dv1
The change of integration variable to
β = (v1 − u1 ) m 2k B T( )1 2
changes this integral to:
(v1 )ave = 1
π
β 2k B T
m
!
"
# $
%
&
1 2
+ u1
!
"
##
$
%
&&
−∞
+∞
∫ exp −
β 2
{ }d
β = 0 + 1
π u1
π = u1 ,
where the first term of the integrand is an odd function integrated on an even interval so its
contribution is zero. This procedure is readily repeated for the other directions to find (v2 )ave = u2 ,
and (v3 )ave = u3 . Thus, u = (u1 , u2 , u3 ) is the average molecular velocity.
Using the same simplifications and change of integration variables produces:
σ1
2 = m
2
π k B T
!
"
# $
%
&
3 2
(v1 − u1 ) 2
−∞
+∞
∫
−∞
+∞
∫
−∞
+∞
∫ exp − m
2k B T (v1 − u1 ) 2 + (v2 − u2 ) 2 + (v3 − u3 ) 2*+ ,-
.
/
0
1
2
3 dv1dv2dv3
= m
2
π k B T
!
"
# $
%
&
1 2
(v1 − u1 ) 2
±∞
+∞
∫ exp − m(v1 − u1 ) 2
2k B T
*
+
,
-
.
/ dv1 = 1
π
2k B T
m
!
"
# $
%
&
β 2
±∞
+∞
∫ exp −
β 2
{ }d
β .

Fluid Mechanics, 6 th Ed. Kundu, Cohen, and Dowling
The final integral over
β is:
€
π 2, so the standard deviations of molecular speed are
€
σ1 = k B T m( )1 2
=
σ 2 =
σ 3 ,
where the second two equalities follow from repeating this calculation for the second and third
directions.
b) From (1.27), n V = p k B T = (101.3kPa) [1.381×10−23 J / K ⋅ 295K ] = 2.487 ×10 25 m−3
c) From n/V from part b):
€
n = 2.487 ×1010 for V = 10 3
μm3 = 10–15 m3
€
n = 2.487 ×10 7 for V = 1.0
μm3 = 10–18 m3
€
n = 2.487 ×10 4 for V = 0.001
μm3 = 10–21 m3
d) From (1.29), the gas constant is R = (kB/m), and R = 287 m2 /s2K for air. Compute:
2
σ a,1 u1 = 2 k B T m n( )1 2
1m / s[ ] = 2 RT n( )1 2
1m / s = 2 287⋅ 295 n( )1 2
= 582 n . Thus,
for V = 10–15 m3 : 2
σ a,1 u1 = 0.00369,
V = 10–18 m3 : 2
σ a,1 u1 = 0.117, and
V = 10–21 m3 : 2
σ a,1 u1 = 3.69.
e) To achieve a relative uncertainty of 1% we need n ≈ (582/0.01) 2 = 3.39
€
×10 9 , and this
corresponds to a volume of 1.36
€
×10 -16 m3 which is a cube with side dimension ≈ 5
μm.

Loading page 6...

Fluid Mechanics, 6 th Ed. Kundu, Cohen, and Dowling
Exercise 1.4. Using the Maxwell molecular speed distribution given by (1.4),
a) determine the most probable molecular speed,
b) show that the average molecular speed is as given in (1.5),
c) determine the root-mean square molecular speed = vrms = 1
n v2 f (v)
0
∞
∫ dv
#
$% &
'(
1 2
,
d) and compare the results from parts a), b) and c) with c = speed of sound in a perfect gas
under the same conditions.
Solution 1.4. a) The most probable speed, vmp, occurs where f(v) is maximum. Thus, differentiate
(1.4) with respect v, set this derivative equal to zero, and solve for vmp. Start from:
f (v) = 4
π n m
2
π k B T
!
"
# $
%
&
3 2
v2 exp − mv2
2k B T
(
)
*
+
,
- , and differentiate
df
dv = 4
π n m
2
π k B T
!
"
# $
%
&
3 2
2vmp exp − mvmp
2
2k B T
(
)
*
+*
,
-
*
.* − mvmp
3
k B T exp − mvmp
2
2k B T
(
)
*
+*
,
-
*
.*
/
0
1
1
2
3
4
4 = 0
Divide out common factors to find:
2 − mvmp
2
k B T = 0 or vmp = 2k B T
m .
b) From (1.5), the average molecular speed v is given by:
v = 1
n v
0
∞
∫ f (v)dv = 4
π m
2
π k B T
#
$
% &
'
(
3 2
v3
0
∞
∫ exp − mv2
2k B T
*
+
,
-
.
/ dv .
Change the integration variable to
β = mv2 2k B T to simplify the integral:
v = 4 m
2
π k B T
!
"
# $
%
&
1 2
k B T
m
β
0
∞
∫ exp −
β{ }d
β = 8k B T
π m
!
"
# $
%
&
1 2
−
βe−
β − e−
β
( )0
∞
= 8k B T
π m
!
"
# $
%
&
1 2
,
and this matches the result provided in (1.5).
c) The root-mean-square molecular speed vrms is given by:
vrms
2 = 1
n v2
0
∞
∫ f (v)dv = 4
π m
2
π k B T
#
$
% &
'
(
3 2
v4
0
∞
∫ exp − mv2
2k B T
*
+
,
-
.
/ dv .
Change the integration variable to
β = v m 2k B T( )1 2
to simplify the integral:
vrms
2 = 4
π
2k B T
m
!
"
# $
%
&
1 2
β 4
0
∞
∫ exp −
β 2
{ }d
β = 4
π
2k B T
m
!
"
# $
%
& 3
π
8 = 3k B T
m .
Thus, vrms = (3kB T/m) 1/2 .
d) From (1.28), R = (kB/m) so vmp = 2RT , v = (8 /
π )RT , and vrms = 3RT . All three speeds
have the same temperature dependence the speed of sound in a perfect gas:
€
c =
γRT , but are
factors of 2
γ , 8
πγ and
€
3
γ , respectively, larger than c.

Loading page 7...

Fluid Mechanics, 6 th Ed. Kundu, Cohen, and Dowling
Exercise 1.5. By considering the volume swept out by a moving molecule, estimate how the
mean-free path, l, depends on the average molecular cross section dimension d and the
molecular number density n for nominally spherical molecules. Find a formula for (the ratio
of the mean-free path to the mean intermolecular spacing) in terms of the nominal molecular
volume ( ) and the available volume per molecule (1/n). Is this ratio typically bigger or smaller
than one?
Solution 1.5. The combined collision cross section for two spherical molecules having diameter
€
d is
€
πd 2 . The mean free path l is the average distance traveled by a molecule between
collisions. Thus, the average molecule should experience one
collision when sweeping a volume equal to
€
πd 2l. If the molecular
number density is n, then the volume per molecule is n–1 , and the
mean intermolecular spacing is n–1/3 . Assuming that the swept volume
necessary to produce one collision is proportional to the volume per
molecule produces:
π d 2l = C n or l = C n
π d 2
( ) ,
where C is a dimensionless constant presumed to be of order unity. The dimensionless version of
this equation is:
mean free path
mean intermolecular spacing = l
n−1 3 = l n1 3
= C
n2 3
π d 2 = C
nd 3
( )2 3 = C n−1
d 3
"
#
$ %
&
'
2 3
= C volume per molecule
molecular volume
"
#
$ %
&
'
2 3
,
where all numerical constants like
π have been combined into C. Under ordinary conditions in
gases, the molecules are not tightly packed so l >> n−1 3 . In liquids, the molecules are tightly
packed so l ~ n−1 3 .
ln1 3
d 3
€
d

Loading page 8...

Fluid Mechanics, 6 th Ed. Kundu, Cohen, and Dowling
Exercise 1.6. Compute the average relative speed, vr , between molecules in a gas using the
Maxwell speed distribution f given by (1.4) via the following steps.
a) If u and v are the velocities of two molecules then their relative velocity is: vr = u – v. If the
angle between u and v is
θ, show that the relative speed is: vr = |vr | = u2 + v2 − 2uv cos
θ where
u = |u|, and v = |v|.
b) The averaging of vr necessary to determine vr must include all possible values of the two
speeds (u and v) and all possible angles
θ. Therefore, start from:
vr = 1
2n2 vr f (u)
all u,v,
θ
∫ f (v)sin
θd
θdvdu ,
and note that vr is unchanged by exchange of u and v, to reach:
vr = 1
n2 u2 + v2 − 2uv cos
θ
θ=0
π
∫
v=u
∞
∫
u=0
∞
∫ sin
θ f (u) f (v)d
θdvdu
c) Note that vr must always be positive and perform the integrations, starting with the angular
one, to find:
vr = 1
3n2
2u3 + 6uv2
uvv=u
∞
∫
u=0
∞
∫ f (u) f (v)dvdu = 16k B T
π
#
$
% &
'
(
1 2
= 2 v .
Solution 1.6. a) Compute the dot produce of vr with itself:
vr
2
= vr ⋅ vr = (u − v)⋅ (u − v) = u ⋅ u − 2u ⋅ v + v ⋅ v = u2 − 2uv cos
θ + v2 .
Take the square root to find: |vr | = u2 + v2 − 2uv cos
θ .
b) The average relative speed must account for all possible molecular speeds and all possible
angles between the two molecules. [The coefficient 1/2 appears in the first equality below
because the probability density function of for the angle
θ in the interval 0 ≤
θ ≤
π is (1/2)sin
θ.]
vr = 1
2n2 vr f (u)
all u,v,
θ
∫ f (v)sin
θd
θdvdu
= 1
2n2 u2 + v2 − 2uv cos
θ f (u)
all u,v,
θ
∫ f (v)sin
θd
θdvdu
= 1
2n2 u2 + v2 − 2uv cos
θ
θ=0
π
∫
v=0
∞
∫
u=0
∞
∫ sin
θ f (u) f (v)d
θdvdu.
In u-v coordinates, the integration domain covers the first
quadrant, and the integrand is unchanged when u and v are
swapped. Thus, the u-v integration can be completed above the
line u = v if the final result is doubled. Thus,
vr = 1
n2 u2 + v2 − 2uv cos
θ
θ=0
π
∫
v=u
∞
∫
u=0
∞
∫ sin
θ f (u) f (v)d
θdvdu .
Now tackle the angular integration, by settingβ = u2 + v2 − 2uv cos
θ so that d
β = +2uvsin
θd
θ . This leads to
vr = 1
n2
β1 2
β=(v−u) 2
(v+u) 2
∫
v=u
∞
∫
u=0
∞
∫ d
β
2uv f (u) f (v)dvdu , u!
v! dv!
du!
u = v!

Loading page 9...

Fluid Mechanics, 6 th Ed. Kundu, Cohen, and Dowling
and the
β-integration can be performed:
vr = 1
2n2
2
3
β 3 2
( )(v−u) 2
(v+u) 2
v=u
∞
∫
u=0
∞
∫ f (u)
u
f (v)
v dvdu = 1
3n2 (v + u)3 − (v − u)3
( )
v=u
∞
∫
u=0
∞
∫ f (u)
u
f (v)
v dvdu .
Expand the cubic terms, simplify the integrand, and prepare to evaluate the v-integration:
vr = 1
3n2 2u3 + 6uv2
( )
v=u
∞
∫
u=0
∞
∫ f (v)
v dv f (u)
u du
= 1
3n 2u3 + 6uv2
( )
v=u
∞
∫
u=0
∞
∫ 4
π
v
m
2
π k B T
#
$
% &
'
(
3 2
v2 exp − mv2
2k B T
*
+
,
-
.
/ dv f (u)
u du.
Use the variable substitution:
α = mv2 /2kB T so that d
α = mvdv/kB T, which reduces the v-
integration to:
vr = 1
3n 2u3 + 6u k B T
m
α
!
"
# $
%
&
mu2 k B T
∞
∫
u=0
∞
∫ 4
π m
2
π k B T
!
"
# $
%
&
3 2
exp −
α{ } k B T
m d
α f (u)
u du
= 2
3n
m
2
π k B T
!
"
# $
%
&
1 2
2u3 + 6u k B T
m
α
!
"
# $
%
&
mu2 k B T
∞
∫
u=0
∞
∫ e−
α d
α f (u)
u du
= 2
3n
m
2
π k B T
!
"
# $
%
&
1 2
−2u3e−
α + 6u k B T
m −
αe−
α − e−
α
( )
!
"
# $
%
&mu2 k B T
∞
u=0
∞
∫ f (u)
u du
= 2
3n
m
2
π k B T
!
"
# $
%
&
1 2
8u3 +12u k B T
m
!
"
# $
%
&
u=0
∞
∫ exp − mu2
2k B T
!
"
# $
%
& f (u)
u du.
The final u-integration may be completed by substituting in for f(u) and using the variable
substitution
γ = u m k B T( )1 2
.
vr = 1
3
2m
π k B T
!
"
# $
%
&
1 2
8 k B T
m
!
"
# $
%
&
3 2
γ 3 +12 k B T
m
!
"
# $
%
&
3 2
γ
!
"
##
$
%
&&
0
∞
∫ 4
π m
2
π k B T
!
"
# $
%
&
3 2
k B T
m
!
"
# $
%
&
γ exp −
γ 2
( ) d
γ
= 2
3
π
k B T
m
!
"
# $
%
&
1 2
8
γ 4 +12
γ 2
( )
0
∞
∫ exp −
γ 2
( ) d
γ = 2
3
π
k B T
m
!
"
# $
%
&
1 2
8 3
8
π +12 1
4
π
!
"
# $
%
&
= 4
π
k B T
m
!
"
# $
%
&
1 2
= 16k B T
π m
!
"
# $
%
&
1 2
= 2v
Here, v is the mean molecular speed from (1.5).

Loading page 10...

Fluid Mechanics, 6 th Ed. Kundu, Cohen, and Dowling
Exercise 1.7. In a gas, the molecular momentum flux (MFij) in the j-coordinate direction that
crosses a flat surface of unit area with coordinate normal direction i is:
MFij = 1
V mvi v j f (v)d3v
all v
∫∫∫ where f(v) is the Maxwell velocity distribution (1.1). For a perfect
gas that is not moving on average (i.e., u = 0), show that MFij = p (the pressure), when i = j, and
that MFij = 0, when i ≠ j.
Solution 1.7. Start from the given equation using the Maxwell distribution:
MFij = 1
V mvi v j f (v)d3v
all u
∫∫∫ = nm
V
m
2
π k B T
"
#
$ %
&
'
3 2
vi v j
−∞
+∞
∫
−∞
+∞
∫
−∞
+∞
∫ exp − m
2k B T v1
2 + v2
2 + v3
2
( )
*
+
,
-
.
/ dv1dv2dv3
and first consider i = j = 1, and recognize
ρ = nm/V as the gas density, as in (1.28).
MF11 =
ρ m
2
π k B T
!
"
# $
%
&
3 2
u1
2
−∞
+∞
∫
−∞
+∞
∫
−∞
+∞
∫ exp − m
2k B T v1
2 + v2
2 + v3
2
( )
*
+
,
-
.
/ dv1dv2dv3
=
ρ m
2
π k B T
!
"
# $
%
&
3 2
v1
2 exp − mv1
2
2k B T
(
)
*
+
,
- dv1
−∞
+∞
∫ exp − mv2
2
2k B T
(
)
*
+
,
- dv2
−∞
+∞
∫ exp − mv3
2
2k B T
(
)
*
+
,
-−∞
+∞
∫ dv3
The first integral is equal to 2k B T m( )3 2
π 2( ) while the second two integrals are each equal to
2
π k B T m( )1 2
. Thus:
MF11 =
ρ m
2
π k B T
!
"
# $
%
&
3 2
2k B T
m
!
"
# $
%
&
3 2
π
2
2
π k B T
m
!
"
# $
%
&
1 2
2
π k B T
m
!
"
# $
%
&
1 2
=
ρ k B T
m =
ρRT = p
where kB/m = R from (1.28). This analysis may be repeated with i = j = 2, and i = j = 3 to find:
MF22 = MF33 = p, as well.
Now consider the case i ≠ j. First note that MFij = MFji because the velocity product under
the triple integral may be written in either order vi vj = vj vi, so there are only three cases of
interest. Start with i = 1, and j = 2 to find:
MF12 =
ρ m
2
π k B T
!
"
# $
%
&
3 2
v1v2
−∞
+∞
∫
−∞
+∞
∫
−∞
+∞
∫ exp − m
2k B T v1
2 + v2
2 + v3
2
( )
*
+
,
-
.
/ dv1dv2dv3
=
ρ m
2
π k B T
!
"
# $
%
&
3 2
v1 exp − mv1
2
2k B T
(
)
*
+
,
- dv1
−∞
+∞
∫ v2 exp − mv2
2
2k B T
(
)
*
+
,
- dv2
−∞
+∞
∫ exp − mv3
2
2k B T
(
)
*
+
,
-−∞
+∞
∫ dv3
Here we need only consider the first integral. The integrand of this integral is an odd function
because it is product of an odd function, v1 , and an even function, exp −mv1
2 2k B T{ } . The
integral of an odd function on an even interval [–∞,+∞] is zero, so MF12 = 0. And, this analysis
may be repeated for i = 1 and j = 3, and i = 2 and j = 3 to find MF13 = MF23 = 0.

Loading page 11...

Fluid Mechanics, 6 th Ed. Kundu, Cohen, and Dowling
Exercise 1.8. Consider the viscous flow in a channel of width 2b. The channel is aligned in the
x-direction, and the velocity u in the x-direction at a distance y from the channel centerline is
given by the parabolic distribution
€
u(y) = U0 1− y b( )2
[ ]. Calculate the shear stress
τ as a
function y,
μ, b, and Uo . What is the shear stress at y = 0?
Solution 1.8. Start from (1.3):
€
τ =
μ du
dy =
μ d
dy U o 1− y
b
$
%
& '
(
)
2*
+
,
-
.
/ = –2
μU o
y
b2 . At y = 0 (the location of
maximum velocity)
τ = 0. At At y = ±b (the locations of zero velocity),
€
τ = 2
μU o b.

Loading page 12...

Fluid Mechanics, 6 th Ed. Kundu, Cohen, and Dowling
Exercise 1.9. Hydroplaning occurs on wet roadways when sudden braking causes a moving
vehicle’s tires to stop turning when the tires are separated from the road surface by a thin film of
water. When hydroplaning occurs the vehicle may slide a significant distance before the film
breaks down and the tires again contact the road. For simplicity, consider a hypothetical version
of this scenario where the water film is somehow maintained until the vehicle comes to rest.
a) Develop a formula for the friction force delivered to a vehicle of mass M and tire-contact area
A that is moving at speed u on a water film with constant thickness h and viscosity
μ.
b) Using Newton’s second law, derive a formula for the hypothetical sliding distance D traveled
by a vehicle that started hydroplaning at speed U o
c) Evaluate this hypothetical distance for M = 1200 kg, A = 0.1 m2 , U o = 20 m/s, h = 0.1 mm, andμ = 0.001 kgm–1 s –1 . Compare this to the dry-pavement stopping distance assuming a tire-road
coefficient of kinetic friction of 0.8.
Solution 1.9. a) Assume that viscous friction from the water layer transmitted to the tires is the
only force on the sliding vehicle. Here viscous shear stress at any time will be
μu(t)/h, where u(t)
is the vehicle's speed. Thus, the friction force will be A
μu(t)/h.
b) The friction force will oppose the motion so Newton’s second law implies: M du
dt = −A
μ u
h .
This equation is readily integrated to find an exponential solution: u(t) = U o exp −A
μt Mh( ) ,
where the initial condition, u(0) = U o, has been used to evaluate the constant of integration. The
distance traveled at time t can be found from integrating the velocity:
x(t) = u( !t )d !t
o
t
∫ = U o exp −A
μ !t Mh( ) d !t
o
t
∫ = U o Mh A
μ( ) 1− exp −A
μt Mh( )$% &' .
The total sliding distance occurs for large times where the exponential term will be negligible so:
D = U o Mh A
μ
c) For M = 1200 kg, A = 0.1 m2 , U o = 20 m/s, h = 0.1 mm, and
μ = 0.001 kgm–1 s –1 , the stopping
distance is: D = (20)(1200)(10–4 )/(0.1)(0.001) = 24 km! This is an impressively long distance and
highlights the dangers of driving quickly on water covered roads.
For comparison, the friction force on dry pavement will be –0.8Mg, which leads to a
vehicle velocity of: u(t) = U o − 0.8gt , and a distance traveled of x(t) = U o t − 0.4gt2 . The vehicle
stops when u = 0, and this occurs at t = U o/(0.8g), so the stopping distance is
D = U o
U o
0.8g
!
"
# $
%
& − 0.4g U o
0.8g
!
"
# $
%
&
2
= U o
2
1.6g ,
which is equal to 25.5 m for the conditions given. (This is nearly three orders of magnitude less
than the estimated stopping distance for hydroplaning.)

Loading page 13...

Fluid Mechanics, 6 th Ed. Kundu, Cohen, and Dowling
Exercise 1.10. Estimate the height to which water at 20°C will rise in a capillary glass tube 3
mm in diameter that is exposed to the atmosphere. For water in contact with glass the contact
angle is nearly 0°. At 20°C, the surface tension of a water-air interface is
σ = 0.073 N/m.
Solution 1.10. Start from the result of Example 1.4.
h = 2
σ cos
α
ρgR = 2(0.073N / m)cos(0°)
(10 3 kg / m3 )(9.81m / s2 )(1.5×10−3 m) = 9.92mm

Loading page 14...

Fluid Mechanics, 6 th Ed. Kundu, Cohen, and Dowling
Exercise 1.11. A manometer is a U-shaped tube containing mercury of density
ρm . Manometers
are used as pressure-measuring devices. If the fluid in tank A has a pressure p and density
ρ, then
show that the gauge pressure in the tank is: p − patm =
ρmgh −
ρga. Note that the last term on the
right side is negligible if
ρ «
ρm . (Hint: Equate the pressures at X and Y.)
Solution 1.9. Start by equating the pressures at X and Y.
p X = p +
ρga = p atm +
ρm gh = p Y.
Rearrange to find:
p – p atm =
ρm gh –
ρga.

Loading page 15...

Fluid Mechanics, 6 th Ed. Kundu, Cohen, and Dowling
Exercise 1.12. Prove that if e(T,
υ) = e(T) only and if h(T, p) = h(T) only, then the (thermal)
equation of state is (1.28) or p
υ = kT, where k is constant.
Solution 1.12. Start with the first equation of (1.24): de = Tds – pd
υ, and rearrange it:
€
ds = 1
T de + p
T dυ =
∂s
∂e
$
%
& '
(
)
υ
de +
∂s
∂υ
$
%
& '
(
) e
dυ ,
where the second equality holds assuming the entropy depends on e and
υ. Here we see that:
€
1
T =
∂s
∂e
#
$
% &
'
(
υ
, and
€
p
T =
∂s
∂υ
$
%
& '
(
) e
.
Equality of the crossed second derivatives of s,
€
∂
∂υ
∂s
∂e
$
%
& '
(
)
υ
$
%
&
'
(
) e
=
∂
∂e
∂s
∂υ
$
%
& '
(
) e
$
%
&
'
(
)
υ
, implies:
€
∂ 1 T( )
∂υ
$
%
& '
(
)
e
=
∂ p T( )
∂e
$
%
& '
(
)
υ
.
However, if e depends only on T, then (∂/∂
υ)e = (∂/∂
υ)T, thus
€
∂ 1 T( )
∂υ
$
%
& '
(
)
e
=
∂ 1 T( )
∂υ
$
%
& '
(
)
T
= 0, so
€
∂ p T( )
∂e
#
$
% &
'
(
υ
= 0, which can be integrated to find: p/T = f1 (
υ), where f1 is an undetermined function.
Now repeat this procedure using the second equation of (1.24), dh = Tds +
υdp.
€
ds = 1
T dh −
υ
T dp =
∂s
∂h
%
&
' (
)
* p
dh +
∂s
∂p
%
&
'
(
)
* h
dp.
Here equality of the coefficients of the differentials implies:
€
1
T =
∂s
∂h
#
$
% &
'
( p
, and
€
−
υ
T =
∂s
∂p
%
&
'
(
)
* h
.
So, equality of the crossed second derivatives implies:
€
∂ 1 T( )
∂p
#
$
%
&
'
(
h
= −
∂ υ T( )
∂h
#
$
%
&
'
(
p
. Yet, if h depends
only on T, then (∂/∂p)h = (∂/∂p)T, thus
€
∂ 1 T( )
∂p
#
$
% &
'
(
h
=
∂ 1 T( )
∂p
#
$
% &
'
(
T
= 0, so
€
−
∂ υ T( )∂h
%
&
' (
)
*
p
= 0, which can
be integrated to find:
υ/T = f2 (p), where f2 is an undetermined function.
Collecting the two results involving f1 and f2 , and solving for T produces:
€
p
f1 (
υ) = T =
υ
f2 ( p) or
€
pf2 ( p) =
υf1 (
υ) = k ,
where k must be is a constant since p and
υ are independent thermodynamic variables.
Eliminating f1 or f2 from either equation on the left, produces p
υ = kT.
And finally, using both versions of (1.24) we can write: dh – de =
υdp + pd
υ = d(p
υ).
When e and h only depend on T, then dh = cpdT and de = cvdT, so
dh – de = (cp – cv )dT = d(p
υ) = kdT , thus k = cp – cv = R,
where R is the gas constant. Thus, the final result is the perfect gas law: p = kT/
υ =
ρRT.

Loading page 16...

13 more pages available. Scroll down to load them.

Preview Mode

100%

Study Now!

XY-Copilot AI

Unlimited Access

Secure Payment

Instant Access

24/7 Support

Document Chat

Document Details

Subject

Mechanical Engineering

Fluid Mechanics , 6th Edition Solution Manual

Study Now!

Document Details

Related Documents

A system is a group of parts that work together to

Solution Manual for Introduction to Robotics: Mechanics and Control, 4th Edition

Solution Manual For Thermal Radiation Heat Transfer, 6th Edition

Solution Manual For Thermodynamics: An Interactive Approach, 1st Edition

Solution Manual for Design of Machinery: An Introduction to the Synthesis and Analysis of Mechanisms and Machines, 5th Edition

Solution Manual For Design Of Machine Elements, 8th Edition

Solution Manual For Applied Strength Of Materials, 5th Edition

Mechanical Vibrations: Theory and Applications 1st Edition Solution Manual

Solution Manual For System Dynamics, 4th Edition

Solution Manual for Machine Elements in Mechanical Design, 6th Edition

Company

Explore

Study Tools