Question: The steam at ( 9 0 0 mathrm { ~m } / mathrm { s } ) enters into a single
The steam at mathrm~mmathrms enters into a single impulse turbine where the blade velocity is mathrm~mmathrms The blades are symmetrical. If the steam is to enter into the blades without any shock, what will be the blade angles? Also calculate i the blade power ii axial thrust iii blade efficiency. Neglect the frictional effects on the blades. Mass flow rate of steam is mathrm~kgmathrms
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