Munson, Young and Okiishi's Fundamentals of Fluid Mechanics, Binder Ready Version
8th Edition
ISBN: 9781119080701
Author: Philip M. Gerhart, Andrew L. Gerhart, John I. Hochstein
Publisher: WILEY
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Chapter 11.2, Problem 11P
(a)
To determine
The ratio of the static pressure to the stagnation pressure.
(b)
To determine
The ratio of the static pressure to the stagnation pressure.
(c)
To determine
The ratio of the static pressure to the stagnation pressure.
(d)
To determine
The ratio of the static pressure to the stagnation pressure.
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This is an old exam practice question.
As shown in the figure below, moist air at T₁ = 36°C, 1 bar, and 35% relative humidity enters a heat exchanger operating at steady state
with a volumetric flow rate of 10 m³/min and is cooled at constant pressure to 22°C. Ignoring kinetic and potential energy effects,
determine:
(a) the dew point temperature at the inlet, in °C.
(b) the mass flow rate of moist air at the exit, in kg/min.
(c) the relative humidity at the exit.
(d) the rate of heat transfer from the moist air stream, in kW.
(AV)1, T1
P₁ = 1 bar
11
= 35%
120
T₂=22°C
P2 = 1 bar
Air at T₁-24°C, p₁-1 bar, 50% relative humidity enters an insulated chamber operating at steady state with a mass flow rate of 3
kg/min and mixes with a saturated moist air stream entering at T₂-7°C, p2-1 bar. A single mixed stream exits at T3-17°C, p3-1 bar.
Neglect kinetic and potential energy effects
Step 1
Your answer is correct.
Determine mass flow rate of the moist air entering at state 2, in kg/min.
m2 = 2.1
Hint
kg/min
Using multiple attempts will impact your score.
5% score reduction after attempt 2
Step 2
Determine the relative humidity of the exiting stream.
Փ3 =
i
%
Attempts: 1 of 3 used
Chapter 11 Solutions
Munson, Young and Okiishi's Fundamentals of Fluid Mechanics, Binder Ready Version
Ch. 11.1 - Prob. 1PCh. 11.1 - Air flows steadily between two sections in a duct....Ch. 11.1 - Consider the flow process in Fig. P11.3. Does the...Ch. 11.1 - Prob. 4PCh. 11.1 - Prob. 5PCh. 11.1 - Prob. 6PCh. 11.1 - Prob. 7PCh. 11.1 - Prob. 8PCh. 11.1 - Air flows in a 15-cm-diameter horizontal pipe. At...Ch. 11.1 - An air heater in a large coal-fired steam...
Ch. 11.2 - Determine the static pressure to stagnation...Ch. 11.2 - Prob. 12PCh. 11.2 - Prob. 13PCh. 11.2 - Prob. 14PCh. 11.2 - Prob. 15PCh. 11.3 - Prob. 16PCh. 11.3 - Prob. 17PCh. 11.3 - Prob. 18PCh. 11.3 - Prob. 19PCh. 11.3 - Prob. 20PCh. 11.3 - Prob. 21PCh. 11.3 - Prob. 22PCh. 11.4 - Prob. 23PCh. 11.4 - Prob. 24PCh. 11.4 - Prob. 25PCh. 11.4 - Prob. 26PCh. 11.4 - Prob. 27PCh. 11.4 - Air flows in a constant-area, insulated duct. The...Ch. 11.5 - Prob. 29PCh. 11.5 - The Pitot tube on a supersonic aircraft (see Video...Ch. 11.5 - An aircraft cruises at a Mach number of 2.0 at an...Ch. 11.5 - Prob. 32PCh. 11.5 - Prob. 33PCh. 11.5 - Prob. 34PCh. 11.5 - Prob. 35PCh. 11.6 - The stagnation pressure and temperature of air...Ch. 11.6 - Prob. 37PCh. 11.6 - Prob. 38PCh. 11.6 - Prob. 39PCh. 11.6 - Prob. 40PCh. 11.6 - Prob. 41PCh. 11.6 - The static pressure to stagnation pressure ratio...Ch. 11.7 - Air flows steadily and isentropically from...Ch. 11.7 - Prob. 44PCh. 11.7 - Prob. 45PCh. 11.7 - Prob. 46PCh. 11.7 - At a certain point in a pipe, air flows steadily...Ch. 11.7 - Prob. 48PCh. 11.7 - Prob. 49PCh. 11.7 - Prob. 50PCh. 11.7 - A jet engine is to be designed for an altitude of...Ch. 11.7 - Prob. 52PCh. 11.7 -
A convergent–divergent nozzle has an exit throat...Ch. 11.7 - An ideal gas flows isentropically through a...Ch. 11.8 - Standard atmospheric air (T0 = 59 F, p0 = 14.7...Ch. 11.8 - Prob. 57PCh. 11.8 - Prob. 58PCh. 11.8 - Prob. 59PCh. 11.8 - Prob. 64PCh. 11.9 - Prob. 66PCh. 11.9 - Prob. 67PCh. 11.9 - Prob. 68PCh. 11.9 - Air enters a frictionless, constant area duct with...Ch. 11.9 - Prob. 70PCh. 11.9 - Prob. 71PCh. 11.9 - Prob. 72PCh. 11.9 - Prob. 73P
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