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Locate the centroid C of the shown element's cross-section.
Considering the flow of a uniform stream of speed V in the x-direction, a source of strength Q at (-1,0) and sink of strength Q at (1,0). Find the velocity potential and the stagnation points
An inventor claims to have developed a refrigeration unit with a COP of 8.5 which maintains the refrigerated space at -10oC while operating in a room where the temperature is 25oC. Can this claim be correct?
a fan at a rock concert is 27 m from the stage where the sound intensity level is 130 db. her eardrums have a diameter
An ideal vapor-compression refrigeration cycle uses r-134a as the working fluid is used to cool a brine solution to -5 C. This solution is pumped to various buildings for the purpose of air conditioning. The refrigerant evaporates at -10 C with a tot..
a pump is being used to transfer water from an open tank p1 0 to one having air at 75 psig p2above the water. if 600
a brayton cycle operates with inlet air at 14 psi and 80f. the turbine inlet temperature is 1800 f and the pressure
Each of the identical rectangular blocks of mass m is homo-geneous with mass center at G. Evaluate () for equilibrium when b = a.
A 0.025 m thick flat plate having a 20 cm X 20 cm cross section is made of plain carbon steel (k=30 W/mC), alpha=32.7 x10^-7m^2/s). The initial plate temperature is 727C. it is cooled by blowing 27C air over the top surface of the plate at 30 m/s; th..
an infinitely long sheet of charge of width l lies in the xy-plane between x - l2 and x l2. the surface charge
Consider a 210 MW steam power plant that operates on a simple ideal Rankine cycle. Steam enters the turbine at 10 MPa and 500o C and is cooled in the condenser to a pressure of 10 kPa. Show the cycle on a T-s diagram with respect to the saturation li..
The available bandwidth in a cluster is 1.25MHz. Find the number of channels per cell for the following systems:
Develop a program that performs an energy rate balance on a gas turbine engine.- Input the appropriate gas properties (in the proper units), the turbine's heat loss or gain rate.
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