The pressures in Problem 2.27 are now 90 kPa aboard the plane and I 01 kPa at
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The pressures in Problem 2.27 are now 90 kPa aboard the plane and I 01 kPa at ground level. What is the plane's altitude if the average air density is 1.19 kg/m ³ and g = 9.8 m/s² ?
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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