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A jet of cross-sectional area A1 steadily issues fluid density at a velocity V1, into a duct of area A2=5A1, as shown in the illustration below. The jet has parallel streamlines. The surrounding flow in the duct as the same density and a velocity V2=(1/2) V2 .The flow mixes thoroughly, and by section B the flow is approximately uniform across the duct area. In terms of p and V1, find the average velocity of flow at section B, and the pressure difference between sections A and B.
The diameter of the tube is 13 cm and its length is 60 m. Determine the overall heat transfer coefficient of this heat exchanger using (a) LMTD and (b) -NTU method.
make a text file that contains what is your absolute path, and call it paths.txt
Use cold air properties to find the highest cycle pressure, the specific energy added by combustion, and the mean effective pressure.
Write a complete program consisting of a Main Program and Subprogram (you choose which type, but there should be only one) that fulfills the following requirements.
The bent rod ABDE is supported by ball-and- socket joint at A and E and by the cable DF. If a 600-N load is applied at C as shown , determine the tension in the cable.
piston cylinder device contains 0.06 m3 of saturated water vapor at 350 KPa pressure. Determine the temperature and the mass of the vapor in.
We're asked to determine the deflection of a beam location for a 2000N load. However the force is directed up the corner NOT centroid.
Determine the phase or phases in a system consisting of H2O at the following conditions and sketch p-v and T-v diagrams shown the locations of each state?
Select the proper heat exchanger from American Industrial Heat Transfer Inc. company. Check whether the pressure drop on the shell side is within allowable pressure drop of 20 psi.
Effect of pressure on temperature and density of air for an adiabatic process, The pressure is to be raised from atmospheric to 7 psi (4.83 bar). The process is adiabatic, and the volume is constant and unknown.
Bypass air exits at 600 m/s while combustion air exits at 1000 m/s. What is the thrust in kN of this engine?
You have a bevel gear and shaft and you have to find the maximum load that can be applied on it.
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