Air flows at 200 m/s through the pipe. The temperature is 500 K and the absolute stagnation pressure is 200 kPa. Assume isentropic flow. For air R = 286.9 J/[kg · K] and k = 1.40. (Figure 1) 0.3 m Determine the Mach number of the flow. Express your answer using three significant figures. M = Determine the mass flow. Express your answer using three significant figures.
Air flows at 200 m/s through the pipe. The temperature is 500 K and the absolute stagnation pressure is 200 kPa. Assume isentropic flow. For air R = 286.9 J/[kg · K] and k = 1.40. (Figure 1) 0.3 m Determine the Mach number of the flow. Express your answer using three significant figures. M = Determine the mass flow. Express your answer using three significant figures.
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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![Air flows at 200 m/s through the pipe. The temperature is 500 K and the absolute
stagnation pressure is 200 kPa. Assume isentropic flow. For air R = 286.9 J/kg · K] and
k = 1.40. (Figure 1)
0.3 m
Determine the Mach number of the flow.
Express your answer using three significant figures.
M =
Determine the mass flow.
Express your answer using three significant figures.
m =
kg/s](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2Fd6dd7fe4-0145-479e-886b-6537235bde89%2F85d0d093-6690-480e-961a-9f8c727310d4%2Faib5wch_processed.png&w=3840&q=75)
Transcribed Image Text:Air flows at 200 m/s through the pipe. The temperature is 500 K and the absolute
stagnation pressure is 200 kPa. Assume isentropic flow. For air R = 286.9 J/kg · K] and
k = 1.40. (Figure 1)
0.3 m
Determine the Mach number of the flow.
Express your answer using three significant figures.
M =
Determine the mass flow.
Express your answer using three significant figures.
m =
kg/s
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