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Figure provides steady-state test data for a steam turbine operating with negligible heat transfer with its surroundings and negligible changes in kinetic and potential energy. A faint photocopy of the data sheet indicates that the power developed is either 3080 or 3800 horsepower. Determine if either or both of these power values can be correct.
one u.s. gallon is equivalent to 0.1337 ft3 1 ft is equivalent to 0.3048 m and 1000ml are equivalent to m3. by using
Air enters a window air conditioner at 1 atm, 32C, 70% relative humidity at a rate of 2 m^3/min, and it leaves as saturated air at 15C. Part of the moisture in the air that condenses during the process is also removed at 15C. Determine the rates of h..
Calculate the number of vacancies per cubic meter in some metal at 753°C. The energy for vacancy formation is 0.81 eV/atom, while the density and atomic weight for this metal are 6.38 g/cm3 and 49.43 g/mol, respectively. Find in m^-3 units.
two steel e30000 ksi pipes 1 and 2 are connected at flange b. pipe 1 has an outside diameter of 6.625 in. and a wall
an airplane flying at m0 0.8 under standard sea level conditions has instrumentation embedded at the stagnation point
Choose and estimate all the design characteristics of the motor, finally display all the power flow diagram results including efficiency and speed regulation of the motor. Give all assumptions taken.
determine the actual and minimum theoretical operating costs, each in $/day.
Consider a three stage compression process with inter cooling, and determine the intermediate pressures that minimize the total work input. How can you generalize this to n-stage compression with inter cooling?
the acceleration of a particle is defined by a kt2. knowing that v -4 ms at t0 and v20 ms at t 4 determine the
an airplane heads west at a 400 km per hour in a 50-km-per-hour northwest wind. find a vector that models the resulting
A piston-cylinder device initially contains 50L of liquid water at 40 degrees C and 200kPa. Heat is transferred to the water at constant pressure until entire liquid is vaporized.
a converging-diverging nozzle has a design mach number of 2.0 . the stagnation pressure at the nozzle inlet is 100
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