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The inlet velocity, pressure and temperature at the compressor for a turbo-jet engine are 275 feet per second, 7 psia and -30 degrees farenheit. the pressure at the compressor outlet is 70 psia. Temperature limit for the engine is 1800 degrees farenheit. Assuming the compression and expansion processes are isentropic calculate the thrust for 1 lbm per second of air flow, the power in horsepower of the thrust and the heat input per lbm of air. Assume constant specific heat and neglect the velocity coming out of the turbine.
What is the discharge revised discharge pressure (guage pressure) of the compressor ? Is the assumption of change in temperature valid for calculating the discharge pressure of the compressor ?
estimate the activation energy for creep for the low carbon nickel alloy using the following temperature dependence of
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
0.2 m3 of saturated liquid r-134a in a piston cylinder is heated at a constant pressure of 800kpa to 50 dcg c. what is
water flows at a rate of 20 ls through a horz pipe dia .03 m. the pressure drop across the valve in the pipe is
a stream of refrigerant-134a at 1 mpa and 12 c is mixed with another stream at 1 mpa and 60 c. if the mass flow rate of
the water level in a sealed tank is 26 m above the ground. the pressure in the air space above the water is 0.25 mpa
How transformations affect the microstructure and mechanical properties of steel.
question1a piston cylinder device contains 25 g of saturated water vapor that is maintained at constant pressure of 300
Calculate the crack length after cycles and subjected to a cyclic stress normal to the crack
a solid cylinder has a mass of 5kg a diameter of 9cm and is 60cm high. it starts at point a and must be moving at 2ms
the volume flow rate of metal into a mold is .025m3min. the top of the sprue has a diameter of 20mm and its length is
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