Engineering
Engineering, 12.04.2020 19:16, reginaakerson230

The following figure shows a supersonic engine inlet design. That engine inlet is being operated at off-design conditions with an inflow Mach number and pressure and temperature of 2.8 and 24 kPa and 200 K, respectively. The lower wall of the inlet turns through an angle of 6° towards the flow while the angle of the upper ramp is 11° towards to the flow.

Determine the flow direction and pressure in region 4 and 4’.
c) Estimate the velocity difference across the slip layer formed between regions 4 and 4’.

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The following figure shows a supersonic engine inlet design. That engine inlet is being operated at...

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