Estimate the stagnation pressure loss across the shock

Reference no: EM131280883

1. Describe what happens to Fanno flow when heat transfer is allowed to occur. Is this the same as a Rayleigh flow with friction considered?

2. The Mach number and stagnation pressure of air are 2.0 and 200 kPa(abs) just upstream of a normal shock. Estimate the stagnation pressure loss across the shock.

Reference no: EM131280883

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