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Air enters a turbine operating at steady state at 500 kPa, 860 K and exits at 100 kPa. A temperature is 460 K. Stray heat transfer and kinetic and potential energy effects are negligible. A hard-to-read photocopy of the data sheet indicates that the pressure of the exiting stream is either 1.0 MPa or 1.8 MPa. Assuming the ideal gas model of air with Cp=1.02 kJ/kg * K, determine if either or both of these pressure values can be correct.
Estimate the temperature of the hottest point in the billet after five minutes of quenching. Neglect end effects; make the calculation for a cylinder of the given diameter but of infinite length.
Find the corresponding damping coefficient c. Identify the system parameters such as the natural frequency and damped frequency. Derive the mathematical expression of the displacement as a function of time with the given initial condition. Plot yo..
the air velocity in a duct is measured by a Pitot-static probe connected to a differential pressure gage. if the air is at 13.4 psia absolute and 70 degrees C and the reading of the differential pressure gage is 0.15 psi, determine the air velocit..
Three springs anda mass are attached to a rigid, weightless bar PQ hinged at one end. How do I find the natural frequency?
what does it mean when a steel cable is required to have a factor of safety of at least 5 against its ultimate load?
Find the volume rate of ?ow in AB, the velocity in BC, the velocity in CD and the diameter of CE.
plot the evolution of the height, h, of the stable boundary layer and the strength, delta thetas, as a function of time.
An uninsulated thin-wall pipe of 75 mm diameter is used to transport water at a temperature of 3?C to an outdoor cooling towe
the 20 mm diameter steel rod bc is attached to the lever ab and to the fixed support c shown in fig 9. the uniform
for flow over a circular cylinder as shown below the velocity outside of boundary layer can be estimated to beux 2
question 1 briefly describe the meaning of the term mechatronics both in terms of the systems approach and the
The die characteristic is Q_x = 0.0015p where p is the head pressure in psi. Determine the flight angle that maximizes the flow rate Q_x and graph it.
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