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If the pressure drop through a cyclone is assumed to be 1 in. of water, estimate the diameter of cyclone required for various air-flow rates to remove 1-in.-diameter aluminum chips
Compute the average density of a solid solution which contains 10 kg of gold, Ag, and 90 kg of silver, Au. The density of pure gold is 19.32 g/cm3 and the density of pure silver is 10.49 g/cm3
a hot water stream at 80 c enters a mixing chamber with a mass flow rate of 0.5 kgs where it is mixed with a stream of
a piston-cylinder device contains 0.1 m3 of liquid water and 0.9 m3 of water vapor in equilibrium at 800 kpa. heat is
The rate of heat addition to an air-standard Brayton cycle is 5.2 × 108 Btu/ h. The pressure ratio for the cycle is 12 and the minimum and maximum temperatures are 520°R and 2800°R, respectively. Determine the thermal efficiency of the cycle.
you are handed an apple that has a mass of 102g. to get a better idea of what different pressures feel like you rig up
Water at 20 C flows across a flat plate at a velocity of 0.25 m/s. compute the distance from the plate’s leading edge to where the laminar boundary layer thickness is 3 cm. Verfiy that the flow is indeed lamiar at this distance.
Presently, benzene vapors are condensed in a heat exchanger using cooling water. The benzene (100 kmol/h) enters at 0.1013 MPa and 120°C, and exits at 0.1013 MPa and 50°C. Cooling water enters at 10°C and exits at 40°C. What is the current demand for..
design an al-si brazing filler alloy that will be used to join an al-mg alloy. the al-mg alloy has a solidus
refrigerant r-134a flows through a refigeration system at a rate of 0.12 kgs . at the entrance to the adiabatic
a gas within a piston-cylinder assembly undergoes a thermodynamic cycle consisting of three processesprocess 1-2
The system shown below is deflected in compression by 6 = 0.014 in. For individual components 1, 2 & 3 find the axial stress in individual component
A large rocket engine delivers hydrogen at 1500°C and 3 MPa to a nozzle with an exit pressure equal to the ambient pressure of 54 kPa. If the thrust of the rocket is 2 MN what is the exit velocity and mass flow rate of hydrogen? (use k = 1.41 and ..
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