Question
The Mach number at point A on tube is measured to be M=2 and the static pressure is 2[Bar] . Downstream at point B, the
The Mach number at point A on tube is measured to be M=2 and the static pressure is 2[Bar] . Downstream at point B, the pressure was measured to be 1.5[Bar]. Calculate the Mach number at point B under the isentropic flow assumption. Also, estimate the temperature at point B. Assume that the specific heat ratio k=1.4 and assume a perfect gas model.
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Thermodynamics An Engineering Approach
Authors: Yunus A. Cengel, Michael A. Boles
8th edition
73398179, 978-0073398174
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