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
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Author:Sadiku, Matthew N. O.
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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
Transcribed Image Text: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
Transcribed Image Text: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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