- An Axial Flow Turbine Stage Has A Flow Coefficient 6 Of 0 65 And The Gas Leaves The Stator Blades At An Angle A Of 1 (100.52 KiB) Viewed 21 times
An axial flow turbine stage has a flow coefficient (6) of 0.65 and the gas leaves the stator blades at an angle (a₁) of
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An axial flow turbine stage has a flow coefficient (6) of 0.65 and the gas leaves the stator blades at an angle (a₁) of
An axial flow turbine stage has a flow coefficient (6) of 0.65 and the gas leaves the stator blades at an angle (a₁) of 65° to the axial direction. If the axial velocity (Ca) is constant and the outlet flow from rotor is axial (a₂= 0), calculate; i. ii. III. iv. The blade loading coefficient (y) The rotor blade relative flow angles (B₁ and ₂) The degree of reaction (R) The total-to-total efficiency (nt(t-1)) marks) (CO3-18 marks)