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Question: Air is expanded from a large reservoir in which the pressure and temperature are 300 kPa and 20°C, respectively, through a convergent-divergent nozzle, which gives an exit Mach number of 1.5. The air from the nozzle flows down a 5-cmdiameter pipe to a reservoir in which the pressure is 140 kPa. A normal shock wave occurs at the end of the pipe. Find the length of the pipe. Discuss what will occur if the pressure in the reservoir at the discharge end of the pipe is decreased. The flow in the nozzle can be assumed to be isentropic and that in the pipe can be assumed to be adiabatic. The friction factor in the pipe can be assumed to be 0.002.
You have two metal specimens both of which are cylindrical with a diameter of 20 mm and a length of 200 mm. One is made of titanium alloy with Young's modulus 100 GPa and the other out of stainless steel Young's modulus 200 GPa. Both are subjected to..
What is the minimum scale ratio of the model that will ensure that its minimum Weber number is 100? Both flows use water at 20°C
Explain intuitively why a quadratic loss function might be preferable to a simple 0 - 1 function (where a part either meets specifications or it doesn't) when assessing quality.
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some engineers have suggested that air compressed into tanks can be used to propel personal transportation vehicles.
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Determine the required development length ld from the point of maximum stress in the bars. Specify the minimum required side cover. Shrinkage and temperature steel is not shown. f′ c = 4000 psi, fy = 60,000 psi.
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