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Steam enters a 10000 hp turbine at 1600 lbf/in^2 and 1400 F, and exits 10 lbf/in^2 and a quality of .9. The measured heat loss from the turbine is 300 BTU/s. Neglect changes in kinetic and potential energy. Determine the requried mass flow rate in (lbm/s).
A 4 m diameter sphere is embedded in insulation. The sphere contains a liquid-ice mixture maintained at 0 deg C. The ambient temperature surrounding the insulation is 25 deg C.
a 6.5m tall tank has a rectangular cross?section and is filled with water to a depth of 3.5m. assuming the pressure on
for the following descriptions please write the appropriate form of the heat conduction equation a a cylindrical rod
Prepare a report on the various types of methods available in Australia to protect intellectual property - The strategy's main items should include what to protect, what countries to protect it in, how to protect it, and when to seek protection
Hydrostatic relation, An empirical formula relating pressure and density for seawater w/ temperature held constant is
A steady flow air compressor compresses 50 lb/min from 14 psia and 80 degrees F to a discharge state at 45 psia and 300 degrees F. Heat departs from the air only via circulating water that enters the jacket at 75 degrees F and leaves at 95 degrees..
a collar having a mass of 0.75 kg and negligible size slides over the surface of a horizontal circular rod for which
water gate is hinged at point o. angle between the gate and the ground is given alpha 60 degrees. the gate opens when
The temperature on the faces of a plane wall 15cm thick are 375 and 85?.The wall is constructed of a special glass with the following properties:k=0.78W/m·?,ρ=2700Kg/m³,Cp=0.84KJ/Kg·?.What is the heat flow through the wall at steady-state cond..
just after launch from the earth the space-shuttle orbiter is in the 28 x 168-mi orbit shown. at the apogee point a its
What information has to be obtained in order to ensure that the method will be a satisfactory one and determine changes in composition of a fluid. Define what is meant by refractive index, and give the relationship between the incident and refracte..
Bypass air exits at 600 m/s while combustion air exits at 1000 m/s. What is the thrust in kN of this engine?
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