Q1) Air at Mach number 2.0, pressure of 80kPa and temperature of 280K is flowing through a convergent divergent diffuser with dimension shown in fig. For certain operation condition shock is found at area of 22cm2. Find the following. A. Throat Mach number B. Exit Mach Number, and the mass flow rate Me2.0 C. If the throat area is change to 8cm, what will happen to the flow structure at the diffuser inlet? D. Calculate the mass flow and sketch the pressure distribution along convergent divergent part. P=80KPa, T-280K At13cm Ai-20cm As-22cm Ae=30cm

Elements Of Electromagnetics
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ISBN:9780190698614
Author:Sadiku, Matthew N. O.
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Q1) Air at Mach number 2.0, pressure of 80kPa and temperature of 280K is flowing through a
convergent divergent diffuser with dimension shown in fig. For certain operation condition
shock is found at area of 22cm2. Find the following.
A. Throat Mach number
B. Exit Mach Number, and the mass flow rate
C. If the throat area is change to 8cm, what will
happen to the flow structure at the diffuser inlet?
D. Calculate the mass flow and sketch the pressure
distribution along convergent divergent part.
Moo=2.0
P=80kPa,
T-280K
At=13cm
Ai-20cm
As=22cm
Ae=30cm
Transcribed Image Text:Q1) Air at Mach number 2.0, pressure of 80kPa and temperature of 280K is flowing through a convergent divergent diffuser with dimension shown in fig. For certain operation condition shock is found at area of 22cm2. Find the following. A. Throat Mach number B. Exit Mach Number, and the mass flow rate C. If the throat area is change to 8cm, what will happen to the flow structure at the diffuser inlet? D. Calculate the mass flow and sketch the pressure distribution along convergent divergent part. Moo=2.0 P=80kPa, T-280K At=13cm Ai-20cm As=22cm Ae=30cm
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