Engineering, 14.09.2019 01:30, drepeter86
Atmospheric air enters the intake diffuser of a jet aircraft flying at a mach number of 0.8 at a constant altitude where the static pressure and temperature are 25kpa and 220k, respectively. the entrance area of the intake is 0.5m2 and the area at entry to the compressor is 0.8 m2. there is a loss of 10% of the stagnation pressure of the air as it flows to the compressor. using compressible flow theory and assuming adiabatic flow in the intake, determine the mach number and velocity of the flow entering the compressor.
Answers: 1
Engineering, 04.07.2019 19:10, netflixacc0107
What is the major difference between thermoplastics and thermosetting plastics from the polymerization structure point of view?
Answers: 2
Engineering, 04.07.2019 19:20, carterdaw
Aseries piping system conveys methyl alcohol. the system consists of 70 m of 1- nominal pipe follow by 50 m of 2-nominal pipe, both schedule 40 commercial steel. the 1-nominal pipe contains 3 90° elbows (regular) anda fully open gate valve, all threaded. the pressure drop through the system is 150 kpa. determine the volume flow rate through the system that is horizontally laid.
Answers: 1
Engineering, 06.07.2019 03:20, Anonymous7170
Explain in your own word the concept of a solid solution, in alloys, and how it can be created.
Answers: 3
Atmospheric air enters the intake diffuser of a jet aircraft flying at a mach number of 0.8 at a con...
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