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Fluid Mechanics
8th Edition
ISBN: 9780073398273
Author: Frank M. White
Publisher: McGraw-Hill Education
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Question
Chapter 5, Problem 5.77P
To determine
(a)
The expected flow rate of the model.
To determine
(b)
The danger of using only Froude scaling for this test.
To determine
(c)
To derive: a formula for a force on the model as compared to the force on the prototype.
Expert Solution & Answer
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Students have asked these similar questions
|The typical cruising altitude of a commercial jet airliner is 10,700 m above
sea level where the local atmospheric temperature is 219 K, and the pressure
is 0.25 bar. The aircraft utilizes a cold air-standard Brayton cycle as shown
with a volume flow rate of 1450 m³/s. The compressor pressure ratio is 50,
and the maximum cycle temperature is 1700 K. The compressor and turbine
isentropic efficiencies are 90%. Neglect kinetic and potential energy effects
in this problem. Assume constant specific heats with k=1.4, Ra=0.287 kJ/kg-
K, Cp=1.0045 kJ/kg-K, and cv = 0.7175 kJ/kg-K.
a) Draw a T-s diagram for this cycle on the diagram provided.
b) Fill in the table below with the missing information.
T[K]
Heat exchanger
Heat exchanger
State
P [bar]
1
0.25
2s
2
3
4s
4
Turbine
c) (5pts) Determine the inlet air density in [kg/m³] (at state 1), and the system mass flowrate
in [kg/s].
d) (10pts) Determine the net power developed in [MW]. Be sure to draw each component you
are analyzing, define the…
On the axis provide, draw a corresponding T-s diagram for the Brayton cycle shown given
the following information:
iv.
V.
vi.
Compressor 1 is reversible, but Compressor 2 and the turbine are irreversible.
The pressure drops through the regenerator are combustors are negligible.
The pressures at state (1) and state (10) are equal to the atmospheric pressure.
T
8
Regenerator
fmm
mmm
Qin
Combustor
Compressor
Compressor
Turbine
W
cycle
Intercooler
mm
Cour
For parts a) through e), consider the two power cycles shown in the diagram at the right, Cycle A:
1-2-3-4-1, and Cycle B: 1-2-3-4-1.
a) What type of power cycles are shown?
b) Which of cycles has a higher efficiency?
c) Which of the cycles has a higher work output?
d) For either cycle, would increasing the maximum cycle temperature
(3) increase or decrease the efficiency?
Cycle A: 1-2-3-4-1
3
3
Cycle B: 1-2-3-4-1
1
e) For either cycle, would decreasing the minimum cycle temperature
(1) increase or decrease the efficiency?
f) On the axis provide, draw a corresponding T-s diagram for the Rankine cycle shown given
the following information:
i. All turbines and pumps in the system are irreversible.
ii.
111.
The turbine inlet conditions (states 1 and 2) are superheated, while the 2nd stage
turbine outlet is a saturated mixture.
The condenser outlet state (4) and the CFWH outlet state (7) are saturated liquid.
2
Steam
generator
Condenser
www
Closed
feedwater
heater
(1-y)
T
Pump
Trap
8
(y)
S
Chapter 5 Solutions
Fluid Mechanics
Ch. 5 - Prob. 5.1PCh. 5 - A prototype automobile is designed for cold...Ch. 5 - P5.3 The transfer of energy by viscous dissipation...Ch. 5 - When tested in water at 20°C flowing at 2 m/s, an...Ch. 5 - P5.5 An automobile has a characteristic length and...Ch. 5 - P5.6 The disk-gap-band parachute in the...Ch. 5 - Prob. 5.7PCh. 5 - Prob. 5.8PCh. 5 - The Richardson number, Ri, which correlates the...Ch. 5 - Prob. 5.10P
Ch. 5 - Prob. 5.11PCh. 5 - The Stokes number, St, used in particle dynamics...Ch. 5 - Prob. 5.13PCh. 5 - Flow in a pipe is often measured with an orifice...Ch. 5 - The wall shear stress T in a boundary layer is...Ch. 5 - P5.16 Convection heat transfer data are often...Ch. 5 - If you disturb a tank of length L and water depth...Ch. 5 - Prob. 5.18PCh. 5 - Prob. 5.19PCh. 5 - Prob. 5.20PCh. 5 - Prob. 5.21PCh. 5 - As will be discussed in Chap. 11, the power P...Ch. 5 - The period T of vibration of a beam is a function...Ch. 5 - Prob. 5.24PCh. 5 - The thrust F of a propeller is generally thought...Ch. 5 - A pendulum has an oscillation period T which is...Ch. 5 - Prob. 5.27PCh. 5 - Prob. 5.28PCh. 5 - P5.29 When fluid in a pipe is accelerated linearly...Ch. 5 - Prob. 5.30PCh. 5 - P5.31 The pressure drop per unit length in...Ch. 5 - A weir is an obstruction in a channel flow that...Ch. 5 - Prob. 5.33PCh. 5 - Prob. 5.34PCh. 5 - Prob. 5.35PCh. 5 - Prob. 5.36PCh. 5 - Prob. 5.37PCh. 5 - Prob. 5.38PCh. 5 - Prob. 5.39PCh. 5 - Prob. 5.40PCh. 5 - A certain axial flow turbine has an output torque...Ch. 5 - When disturbed, a floating buoy will bob up and...Ch. 5 - Prob. 5.43PCh. 5 - Prob. 5.44PCh. 5 - P5.45 A model differential equation, for chemical...Ch. 5 - P5.46 If a vertical wall at temperature Tw is...Ch. 5 - The differential equation for small-amplitude...Ch. 5 - Prob. 5.48PCh. 5 - P5.48 A smooth steel (SG = 7.86) sphere is...Ch. 5 - Prob. 5.50PCh. 5 - Prob. 5.51PCh. 5 - Prob. 5.52PCh. 5 - Prob. 5.53PCh. 5 - Prob. 5.54PCh. 5 - Prob. 5.55PCh. 5 - P5.56 Flow past a long cylinder of square...Ch. 5 - Prob. 5.57PCh. 5 - Prob. 5.58PCh. 5 - Prob. 5.59PCh. 5 - Prob. 5.60PCh. 5 - Prob. 5.61PCh. 5 - Prob. 5.62PCh. 5 - The Keystone Pipeline in the Chapter 6 opener...Ch. 5 - Prob. 5.64PCh. 5 - Prob. 5.65PCh. 5 - Prob. 5.66PCh. 5 - Prob. 5.67PCh. 5 - For the rotating-cylinder function of Prob. P5.20,...Ch. 5 - Prob. 5.69PCh. 5 - Prob. 5.70PCh. 5 - The pressure drop in a venturi meter (Fig. P3.128)...Ch. 5 - Prob. 5.72PCh. 5 - Prob. 5.73PCh. 5 - Prob. 5.74PCh. 5 - Prob. 5.75PCh. 5 - Prob. 5.76PCh. 5 - Prob. 5.77PCh. 5 - Prob. 5.78PCh. 5 - Prob. 5.79PCh. 5 - Prob. 5.80PCh. 5 - Prob. 5.81PCh. 5 - A one-fiftieth-scale model of a military airplane...Ch. 5 - Prob. 5.83PCh. 5 - Prob. 5.84PCh. 5 - *P5.85 As shown in Example 5.3, pump performance...Ch. 5 - Prob. 5.86PCh. 5 - Prob. 5.87PCh. 5 - Prob. 5.88PCh. 5 - P5.89 Wall friction Tw, for turbulent flow at...Ch. 5 - Prob. 5.90PCh. 5 - Prob. 5.91PCh. 5 - Prob. 5.1WPCh. 5 - Prob. 5.2WPCh. 5 - Prob. 5.3WPCh. 5 - Prob. 5.4WPCh. 5 - Prob. 5.5WPCh. 5 - Prob. 5.6WPCh. 5 - Prob. 5.7WPCh. 5 - Prob. 5.8WPCh. 5 - Prob. 5.9WPCh. 5 - Prob. 5.10WPCh. 5 - Given the parameters U,L,g,, that affect a certain...Ch. 5 - Prob. 5.2FEEPCh. 5 - Prob. 5.3FEEPCh. 5 - Prob. 5.4FEEPCh. 5 - Prob. 5.5FEEPCh. 5 - Prob. 5.6FEEPCh. 5 - Prob. 5.7FEEPCh. 5 - Prob. 5.8FEEPCh. 5 - In supersonic wind tunnel testing, if different...Ch. 5 - Prob. 5.10FEEPCh. 5 - Prob. 5.11FEEPCh. 5 - Prob. 5.12FEEPCh. 5 - Prob. 5.1CPCh. 5 - Prob. 5.2CPCh. 5 - Prob. 5.3CPCh. 5 - Prob. 5.4CPCh. 5 - Does an automobile radio antenna vibrate in...Ch. 5 - Prob. 5.1DPCh. 5 - Prob. 5.2DP
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