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Flow through axial-flow turbo machine rotors can often be assumed axisymmetric i.e. velocity components do not change around the rotor circumference either at inlet or at outlet. Not strictly true as wakes formed behind rotor blades(and inlet guide vanes) which sometimes cannot be ignored. be ignored.
Flow through a rotor, affected both by theinter blade passage geometry and the rotorgeometry Rotation can always be expressed by geometry. Rotation can always be expressed by 3 velocity components:
(i) fluid absolute velocity V
(ii) fluid velocity relative torotor w
(iii) rotor circumferential velocity U
hardness calculatios
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1. Briefly explain how to conduct a market segmentation analysis for an organization. Answer: There are a number of ways by which the market segmentation analysis of an organizatio
All fluids are to some extent compressible but gases show significant changes in density if pressure and/or temperature is changed. Some gas flows can be treated as being incomp
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