- #1
zigggy23
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Homework Statement
At point A in the flow of a compressible fluid, the flow speed is 100 m s−1 and the Mach number of the flow is 0.6. Find (i) the maximum possible flow speed on the streamline through A, and (ii) the flow speed at a point where the pressure has fallen to half its value at point A. Assume the flow to be adiabatic, with index γ = 1.4
Homework Equations
bernoulli's equation for compressible flow & the mach relations
The Attempt at a Solution
I've done part a and I've been playing around with bernoulli's equation and the Mach relations found here https://www.grc.nasa.gov/www/k-12/airplane/isentrop.html for a few hours now. If anyone can help with part b would be much appreciated.