An aircraft is flying at an altitude where the ambient pressure and temperature are 35 kPa and
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Question:
An aircraft is flying at an altitude where the ambient pressure and temperature are 35 kPa and -15C, respectively. The freestream velocity is 1200 km/hr. The inlet diffuser (A2 / A1 = 1.3) slows the air to 85 m/s. Assuming air behaves as an idea gas and constant gas properties, what are the static pressure and temperature of the air at the exit to the diffuser?
Related Book For
Fundamentals of Thermodynamics
ISBN: 978-0471152323
6th edition
Authors: Richard E. Sonntag, Claus Borgnakke, Gordon J. Van Wylen
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