Principles of Heat Transfer (Activate Learning with these NEW titles from Engineering!)
8th Edition
ISBN: 9781305387102
Author: Kreith, Frank; Manglik, Raj M.
Publisher: Cengage Learning
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Textbook Question
Chapter 5, Problem 5.3P
Evaluate the Nusselt number for flow over a sphere for the following conditions:
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Calculate the Moment About the Point A
-20"-
5 lb
40 N
D
1.5 m
40 N
4.5 m
A
15 lb.
150 mm
52 N
5
12
100 mm
15 lb.
26 lb.
12
5
34 lb.
13
8
15
77777
36 lb.
Calculate the Moment About the Point A
-20"-
5 lb
40 N
D
1.5 m
40 N
4.5 m
A
15 lb.
150 mm
52 N
5
12
100 mm
15 lb.
26 lb.
12
5
34 lb.
13
8
15
77777
36 lb.
Formala for Hunzontal component= + cos &
Vertical Component: Fsin t
Find the vertical and horizontal components for the figure bellow:
30°
200 N
77
200 cos 30 = 173 N
//
200 sin 30 = 100 N
YA
a₂+b₂
b₂
(b₁,b₂)
a+b
20haits
(a+b₁,a+b) Magnitude a and b
a = lbl = 2o unite
rugle of vector a wt Horisontal Axis = 30
11 vector & wt Honzontal Axis - 60°
b
b
a= |a|
Cas 30
a2
(a1, a2)
ag = 10
bx = /b/ cos
a
1
20 cos 80 = 17.32
Sia 30 = 20 sin 30.
60
= 10
= 20 Cos 60 = It
by = 161 sin 60 = 20 sia 60 = 17.32
b₁
Rx
ax +bx = 17.32 +10=2732
a₁
a₁+b₁
X
By = ou + by=
+
+ by = 10 + 17.32 =27.32
Magnitude
=
38.637
Find the Vector a +b
the Resultans
The angle of the vector with the horizontal axle is 30 degrees while the angle of the
vector b is 60 degrees.
The magnitude of both vectors is 20 (units)
angle of the Resultant vector
=
tam- " (14)
45
Chapter 5 Solutions
Principles of Heat Transfer (Activate Learning with these NEW titles from Engineering!)
Ch. 5 - Evaluate the Reynolds number for flow over a tube...Ch. 5 - 5.2 Evaluate the Prandtl number from the following...Ch. 5 - Evaluate the Nusselt number for flow over a sphere...Ch. 5 - 5.4 Evaluate the Stanton number for flow over a...Ch. 5 - Evaluate the dimensionless groups hcD/k,UD/, and...Ch. 5 - 5.6 A fluid flows at 5 over a wide, flat plate 15...Ch. 5 - 5.7 The average Reynolds number for air passing in...Ch. 5 - Prob. 5.8PCh. 5 - When a sphere falls freely through a homogeneous...Ch. 5 - 5.10 Experiments have been performed on the...
Ch. 5 - 5.13 The torque due to the frictional resistance...Ch. 5 - The drag on an airplane wing in flight is known to...Ch. 5 - 5.19 Suppose that the graph below shows measured...Ch. 5 - Engine oil at 100C flows over and parallel to a...Ch. 5 - For flow over a slightly curved isothermal...Ch. 5 - Air at 20C flows at 1 m/s between two parallel...Ch. 5 - Air at 1000C flows at an inlet velocity of 2 m/s...Ch. 5 -
5.43 A refrigeration truck is traveling at 130...Ch. 5 - The air-conditioning system in a Chevrolet van for...Ch. 5 - Determine the rate of heat loss from the wall of a...
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