Air is flowing isentropically through a converging duct which is fed from a large reservoir where the temperature and pressure are 350 K and 250 kPa, respectively. At a certain point along the duct, where the cross-sectional area is 0.005 m, the Determine the Mach number, temperature pressure is 150 kPa. and velocity at that point and also calculate the mass flow rate. (Ans: 330.1 K, 0.549, 162.8 kPa, 1.718 kg-s').

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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1. Air is flowing isentropically through a
converging duct which is fed from a large
reservoir
where
the temperature
and
pressure
are
350
K
and
250
КРа,
respectively. At a certain point along the
duct, where the cross-sectional area is
0.005 m,
Determine the Mach number, temperature
the
pressure
is
150
kPa.
and velocity at that point and also calculate
the mass flow rate. (Ans: 330.1 K, 0.549,
162.8 kPa, 1.718 kg-s).
2. Air is supplied to a converging nozzle from a
large reservoir where the temperature and
pressure are 400 K and 100 kPa, respectively.
At a certain cross-section, the temperature
and pressure are measured to be 383.8 K and
63 kPa, respectively. Assuming isentropic
flow, find the Mach number at this cross-
section and the mass flow rate per unit area.
(Ans: 0.46, 103.3 kg-s1-m?).
3. A converging nozzle is fed with air from a
large reservoir where the temperature and
pressure are 400 K and 170 kPa, respectively.
The nozzle has an exit cross-sectional area of
0.001 m? and discharges into the atmosphere
with a pressure of 100 kPa. The flow is
isentropic throughout the nozzle. Determine
the pressure, Mach number, temperature and
velocity at the exit plane, and also find the
mass flow rate. (Ans: 100 kPa, 0.9, 344.8 K,
334.8 m-s", 0.3388 kg-s).
4
A converging nozzle is fed with air from a
Transcribed Image Text:1. Air is flowing isentropically through a converging duct which is fed from a large reservoir where the temperature and pressure are 350 K and 250 КРа, respectively. At a certain point along the duct, where the cross-sectional area is 0.005 m, Determine the Mach number, temperature the pressure is 150 kPa. and velocity at that point and also calculate the mass flow rate. (Ans: 330.1 K, 0.549, 162.8 kPa, 1.718 kg-s). 2. Air is supplied to a converging nozzle from a large reservoir where the temperature and pressure are 400 K and 100 kPa, respectively. At a certain cross-section, the temperature and pressure are measured to be 383.8 K and 63 kPa, respectively. Assuming isentropic flow, find the Mach number at this cross- section and the mass flow rate per unit area. (Ans: 0.46, 103.3 kg-s1-m?). 3. A converging nozzle is fed with air from a large reservoir where the temperature and pressure are 400 K and 170 kPa, respectively. The nozzle has an exit cross-sectional area of 0.001 m? and discharges into the atmosphere with a pressure of 100 kPa. The flow is isentropic throughout the nozzle. Determine the pressure, Mach number, temperature and velocity at the exit plane, and also find the mass flow rate. (Ans: 100 kPa, 0.9, 344.8 K, 334.8 m-s", 0.3388 kg-s). 4 A converging nozzle is fed with air from a
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