At a certain point in a pipe, air flows steadily with a velocity of 150 m/s and has a static pressure of 50 kPa and a static temperature of 4°C. The flow is adiabatic and frictionless. Calculate the maximum possible reduction in area and the following quantities for that minimum area: stagnation pressure, stagnation temperature, static pressure, static temperature, velocity, and Mach number. maximum reduction= % Po2 = To= T₂ = V₂ = kPa K kPa K m/s

At a certain point in a pipe, air flows steadily with a velocity of 150 m/s and has a static pressure of 50 kPa and a static temperature of 4°C. The flow is adiabatic and frictionless. Calculate the maximum possible reduction in area and the following quantities for that minimum area: stagnation pressure, stagnation temperature, static pressure, static temperature, velocity, and Mach number. maximum reduction= % Po2 = To= T₂ = V₂ = kPa K kPa K m/s

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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Question

100%

At a certain point in a pipe, air flows steadily with a velocity of 150 m/s and has a static pressure of 50 kPa and a static temperature of
4°C. The flow is adiabatic and frictionless.
Calculate the maximum possible reduction in area and the following quantities for that minimum area: stagnation pressure,
stagnation temperature, static pressure, static temperature, velocity, and Mach number.
maximum reduction= i
%
Po2 =
To2 =
P2 =
T₂ =
V₂ =
Ma₂ =
i
i
i
kPa
K
kPa
K
m/s

Calculate the quantities listed in (a) at a point where the area is 15% smaller than the initial area.
Po2 =
kPa
To₂ = i
P2 = i
T₂ =
V₂ =
Ma₂ =
i
K
kPa
K
m/s

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