Maurice Tutor

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  • MCS,PHD
    Argosy University/ Phoniex University/
    Nov-2005 - Oct-2011

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    Phoniex University
    Oct-2001 - Nov-2016

Category > Management Posted 20 Feb 2018 My Price 4.00

inward flow radial turbine

An inward flow radial turbine (see Fig. P5.95) involves a nozzle angle, α1, of 60° and an inlet rotor tip speed, U1, of 6 m/s. The ratio of rotor inlet to outlet diameters is 1.8. The absolute velocity leaving the rotor at section (2) is radial with a magnitude of 12 m/s. Determine the energy transfer per unit mass of fluid flowing through this turbine if the fluid is (a) air, (b) water.

Answers

Maurice Tutor
(5)
Status NEW Posted 20 Feb 2018 10:02 PM My Price 4.00

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