Dry air is inhaled at a rate of lo liter/win through a trachea with a diameter of 2 0 mm and a length of 125 mm . The inner surface of the trachea is at a normal body temperature of 37 ° C and may be assumed to be saturated with water. (a) Assuming steady, fully developed flow in the trachea, estimate the mass transfer convection coefficient. (b) Estimate the daily water loss (liter/day) associated with evaporation in the trachea.
Dry air is inhaled at a rate of lo liter/win through a trachea with a diameter of 2 0 mm and a length of 125 mm . The inner surface of the trachea is at a normal body temperature of 37 ° C and may be assumed to be saturated with water. (a) Assuming steady, fully developed flow in the trachea, estimate the mass transfer convection coefficient. (b) Estimate the daily water loss (liter/day) associated with evaporation in the trachea.
Solution Summary: The author explains the mass transfer convection coefficient and the dynamic viscosity of air at atmospheric pressure.
Dry air is inhaled at a rate of lo liter/win through a trachea with a diameter of
2
0
mm
and a length of
125
mm
. The inner surface of the trachea is at a
normal body temperature of
37
°
C
and may be assumed to be saturated with water.
(a) Assuming steady, fully developed flow in the trachea, estimate the mass transfer convection coefficient.
(b) Estimate the daily water loss (liter/day) associated with evaporation in the trachea.
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.
Question 2
You are an engineer working in the propulsion team for a supersonic civil transport
aircraft driven by a turbojet engine, where you have oversight of the design for the
engine intake and the exhaust nozzle, indicated in Figure Q2a. The turbojet engine can
operate when provided with air flow in the Mach number range, 0.60 to 0.80. You are
asked to analyse a condition where the aircraft is flying at 472 m/s at an altitude of
14,000 m. For all parts of the question, you can assume that the flow path of air through
the engine has a circular cross section.
(a)
← intake
normal
shock
472 m/s
A B
(b)
50 m/s
H
472 m/s
B
engine
altitude: 14,000 m
exhaust nozzle
E
F
exit to
atmosphere
diameter: DE = 0.30 m
E
F
diameter: DF = 0.66 m
Figure Q2: Propulsion system for a supersonic aircraft.
a) When the aircraft is at an altitude of 14,000 m, use the International Standard
Atmosphere in the Module Data Book to state the local air pressure and tempera-
ture. Thus show that the aircraft speed…
يكا
- put 96**
I need a detailed drawing with
explanation
or in wake, and the top edge of
im below the free surface of the water. Determine the hydrothed if
hydrostatic on the
Plot the displacement diagram for a cam with roller follower of diameter 10 mm. The required
motion is as follows;
1- Rising 60 mm in 135° with uniform acceleration and retardation motion.
2- Dwell 90°
3- Falling 60 mm for 135° with Uniform acceleration-retardation motion.
Then design the cam profile to give the above displacement diagram if the minimum circle
diameter of the cam is 50 mm.
=--20125
7357
750 X 2.01
You are working as an engineer in a bearing systems design company. The flow of
lubricant inside a hydrodynamic bearing (µ = 0.001 kg m¯¹ s¯¹) can be approximated
as a parallel, steady, two-dimensional, incompressible flow between two parallel plates.
The top plate, representing the moving part of the bearing, travels at a constant speed,
U, while the bottom plate remains stationary (Figure Q1). The plates are separated by
a distance of 2h = 1 cm and are W = 20 cm wide. Their length is L = 10 cm. By
applying the above approximations to the Navier-Stokes equations and assuming that
end effects can be neglected, the horizontal velocity profile can be shown to be
U
y = +h
У
2h = 1 cm
1
x1
y=-h
u(y)
=
1 dP
2μ dx
-y² + Ay + B
moving plate
-
U
stationary plate
2
I2
L = 10 cm
Figure Q1: Flow in a hydrodynamic bearing. The plates extend a width, W = 20 cm,
into the page.
(a) By considering the appropriate boundary conditions, show that the constants take
the following forms:
A =
U
2h
U
1 dP…
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