GATE AE · 2018 · AE
Question 45: Compressible Flows
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Question 45
AENAT2 marksNeeds review
Air at 50 kPa pressure and 400 K temperature flows in a duct at Mach 3.0. A part of the flow leaks through an opening on the duct wall into the ambient, where the pressure is 30 kPa. The maximum Mach number achieved in the discharge is ______ (accurate to two decimal places). (Ratio of specific heats of air is
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2018AE
GATE AE 2018 · Paper 1
Aerospace Engineering · Original paper archive
- Section
- Aerospace Engineering
- Question type
- Numerical answer (NAT)
- Marks
- 2 marks
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