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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
NOR Gate: Figure shows a further example of a 2 input digital gate, again consisting of two NPN transistors, TR1 and TR2, in a different configuration. When input A and input
Hey ,How are you? I need help in another class , its 1 credit class ( Engineering seminar ), how to choose s.d in this class , , ,so we want describing our project which is ( radi
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write an algorithm to find a number that multiplies your name 10 times
The home work is to make an model based system architecture for an electrical car. in Enterprise Architecture with SysMl language.
Q. Discuss briefly the causes and remedies of Shrinkage cavities casting defects. OR Why shrinkage cavities are caus
RE-HEAT (AFTER BURNING) Re-heat is a system fitted to a gas turbine engine as a means of increasing the total thrust. As much as twice the thrust can be obtained using reheat.
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