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An inward flow radial turbine (see Fig. P12.52) involves a nozzle angle, a1, of 60° and an inlet rotor tip speed, U1, of 9 m/s. The ratio of rotor inlet to outlet diameters is 2.0. The radial component of velocity remains constant at 6 m/s through the rotor, and the flow leaving the rotor at section (2) is without angular momentum. If the flowing fluid is water and the stagnation pressure drop across the rotor is 110 kPa, determine the loss of available energy across the rotor and the efficiency involved.
Balance this system with two weights WA and WB in the planes of W1 and W2, respectively, and at a radial distance of 50 mm. Determine WA and WB, and show their positions.
determine the critical load on a steel column having a square cross section 12 mm on a side with a length of 300 mm.
the molar volume cm3mol of a binary liquid mixture at t and p is given by v 120x170x215x18x2x1x2a find expressions for
Refer to the beam shown and draw complete shear and bending moment diagrams. Show ordinates at key points and indicate magnitude of shear and moment.
Two engineers wish to estimate the distance across a lake. One pounds two rocks together under water on one side of the lake and the other submerges his head and hears a small sound 0.62 s later, as indicated by a very accurate stopwatch. What is ..
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