Air enters the diffuser of an aircraft jet engine at a static pressure of $20 mathrm{kPa}$ and
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Air enters the diffuser of an aircraft jet engine at a static pressure of $20 \mathrm{kPa}$ and static temperature $217 \mathrm{~K}$, and a Mach number of 0.9. The air leaves the diffuser with a velocity of $85 \mathrm{~m} / \mathrm{s}$. Assuming isentropic operation, determine the exit static temperature and pressure.
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Sumit kumar
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QUATERNARY Pursuing M.Tech.(2017-2019) in Electronics and Communication Engg. (VLSI DESIGN) from
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TERTIARY B.Tech. (2012-2016) in Electronics and Communication Engg. from GLBITM Greater Noida
SECONDARY Senior Secondary School Examination (Class XII) in 2012 from R.S.S.Inter College, Noida
ELEMENTARY Secondary School Examination (Class X) in 2010 from New R.J.C. Public School ,Noida
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