A mass transfer Operation is preceded by laminar flow of a gaseous species B through a circular tube that is sufficiently long to achieve a fully developed velocity profile. Once the fully developed condition is reached. The gas enters a section of the tube that is wetted with a liquid film (A). The film maintains a uniform vapor density ρ A,s , along the tube surface. (a) Write the differential equation and boundary conditions that govern the species A mass density distribution, ρ A ( x , r ) , for x > 0 . (b) What is the heat transfer analog to this problem? From this analog, write an expression for the average Sherwood number associated with mass exchange over the region 0 ≤ x ≤ L . (c) Beginning with application of conservation of species to a differential control volume of extent π r o 2 d x , derive an expression (Equation 8.86) that may be used to determine the mean vapor density ρ A , m , o at x = L . (d) Consider conditions for which species B is air at 25 ° C and 1 atm and the liquid him consists of water,also at 25 ° C . The flow rate is m ˙ = 2.5 × 10 − 4 kg/s , and the tube diameter is D = 10 mm . What is the mean vapor density at the tube outlet if L = 1 mm ?
A mass transfer Operation is preceded by laminar flow of a gaseous species B through a circular tube that is sufficiently long to achieve a fully developed velocity profile. Once the fully developed condition is reached. The gas enters a section of the tube that is wetted with a liquid film (A). The film maintains a uniform vapor density ρ A,s , along the tube surface. (a) Write the differential equation and boundary conditions that govern the species A mass density distribution, ρ A ( x , r ) , for x > 0 . (b) What is the heat transfer analog to this problem? From this analog, write an expression for the average Sherwood number associated with mass exchange over the region 0 ≤ x ≤ L . (c) Beginning with application of conservation of species to a differential control volume of extent π r o 2 d x , derive an expression (Equation 8.86) that may be used to determine the mean vapor density ρ A , m , o at x = L . (d) Consider conditions for which species B is air at 25 ° C and 1 atm and the liquid him consists of water,also at 25 ° C . The flow rate is m ˙ = 2.5 × 10 − 4 kg/s , and the tube diameter is D = 10 mm . What is the mean vapor density at the tube outlet if L = 1 mm ?
Solution Summary: The author explains the governing differential equation and boundary conditions for the species.
A mass transfer Operation is preceded by laminar flow of a gaseous species B through a circular tube that is sufficiently long to achieve a fully developed velocity profile. Once the fully developed condition is reached. The gas enters a section of the tube that is wetted with a liquid film (A). The film maintains a uniform vapor density
ρ
A,s
, along the tube surface.
(a) Write the differential equation and boundary conditions that govern the species A mass density distribution,
ρ
A
(
x
,
r
)
,
for
x
>
0
. (b) What is the heat transfer analog to this problem? From this analog, write an expression for the average Sherwood number associated with mass exchange over the region
0
≤
x
≤
L
. (c) Beginning with application of conservation of species to a differential control volume of extent
π
r
o
2
d
x
, derive an expression (Equation 8.86) that may be used to determine the mean vapor density
ρ
A
,
m
,
o
at
x
=
L
. (d) Consider conditions for which species B is air at
25
°
C
and
1 atm
and the liquid him consists of water,also at
25
°
C
. The flow rate is
m
˙
=
2.5
×
10
−
4
kg/s
, and the tube diameter is
D
=
10
mm
. What is the mean vapor density at the tube outlet if
L
=
1
mm
?
Net movement of mass from one location, usually meaning stream, phase, fraction, or component, to another. Mass transfer occurs in many processes, such as absorption, evaporation, drying, precipitation, membrane filtration, and distillation.
Ship construction question. Sketch and describe the forward arrangements of a ship. Include componets of the structure and a explanation of each part/ term.
Ive attached a general fore end arrangement. Simplfy construction and give a brief describion of the terms.
Problem 1
Consider R has a functional relationship with variables in the form
R = K xq xx
using
show that
n
✓ - (OR 1.)
=
i=1
2
Их
Ux2
Ихэ
2
(177)² = ² (1)² + b² (12)² + c² (1)²
2
UR
R
x2
x3
4. Figure 3 shows a crank loaded by a force F = 1000 N and Mx = 40 Nm.
a. Draw a free-body diagram of arm 2 showing the values of all forces, moments, and
torques that act due to force F. Label the directions of the coordinate axes on this
diagram.
b. Draw a free-body diagram of arm 2 showing the values of all forces, moments, and
torques that act due to moment Mr. Label the directions of the coordinate axes on this
diagram.
Draw a free body diagram of the wall plane showing all the forces, torques, and
moments acting there.
d. Locate a stress element on the top surface of the shaft at A and calculate all the stress
components that act upon this element.
e. Determine the principal stresses and maximum shear stresses at this point at A.
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