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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
PROBLEM BASED ON USING CHEBYSCHEV IIR FILTER USING BILINEAR TRANSFORMATION
inverse DIFFFT algorithm
what is thermodynamics??
WHATIS LTE CODING TECHNIQUES USE FOR MOBILE SYSTEM
Power Engine: Power producing engines come in two main forms Turboprop and turboshaft. a. Turboprop Engines. Turboprop engines extract most of the energy from the gas stream
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the nature and importance of the efficient market hypothesis and comment on the implications for managers and investors?
Investment allowance Until a few years ago, a company could charge an amount equal to 25 per cent of the original value of an asset as investment allowance in the period in which
Hi, I require a service which involves finite element modelling on commercial software package "ABAQUS". I am personally not sure how to model this on ABAQUS and thats why I have
In the previous discussion, we investigated the static aeroelastic behaviour of straight (unswept) wings. These wings are characterised by an effective decoupling of wing bending a
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