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Sketched in Fig. P12.10 are the upstream [section (1)] and downstream [section (2)] velocity triangles at the arithmetic mean radius for flow through an axial-flow turbomachine rotor. The axial component of velocity is 50 ft/s at sections (1) and (2).
(a) Label each velocity vector appropriately. Use V for absolute velocity, W for relative velocity, and U for blade velocity.
(b) Are you dealing with a turbine or a fan?
(c) Calculate the work per unit mass involved.
(d) Sketch a reasonable blade section. Do you think that the actual blade exit angle will need to be less or greater than 15°? Why?
Assume the same eight features are used to assess quality
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Referring to the thermal circuit diagram of Figure 9.7 for the thermal storage (Trombe) wall building, construct appropriate thermal circuits for (a) attached sunspace, (b) thermal storage, and (c) direct gain buildings.
2/107 The rigid pole and cross-arm assembly is supported by the three cables shown. A turnbuckle at D is tightened until it induces a tension T in CD of 1.2 kN. Express T as a vector. Does it make any differ- ence in the result which coordinate sy..
Gaseous ethanol (CH3CH2OH, also expressed as C2H5OH) is burned with 200 % of theoretical air at standard conditions. During the combustion process 90% of the Carbon in the fuel is converted to CO2 and 10% is converted to CO. Determine the rate of ..
Draw a force diagram for each mass, showing all relevant coordinates.
an accelerometer was used to measure the vibrations of machinery. the sensor output was acquired during an experiment
consider a fluid of density ? inincompressible laminar flow in a plane narrow slit of lengthl and width w formed by two
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Calculate molar absorptivities for In- and HIn at 485 and 625 nm.
A rocket has an empty weight of 500 lb and carries 300 lb of fuel. If the fuel is burned at the rate of 1.5 lb>s and ejected with a velocity of 4400 ft>s relative to the rocket, determine the maximum speed attained by the rocket starting from rest..
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