A normal compressor stage is designed for an inlet flow angle x1 = 15.8°, reaction R = 0.63, and the flow coefficient =

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A Normal Compressor Stage Is Designed For An Inlet Flow Angle X1 15 8 Reaction R 0 63 And The Flow Coefficient 1 (17.4 KiB) Viewed 39 times

A normal compressor stage is designed for an inlet flow angle x1 = 15.8°, reaction R = 0.63, and the flow coefficient = 0.6. Determine the following a. Blade loading factor b. Show that inlet flow angle to the stator is tan α₂ = 1-R+(4/2) $ c. Show that the inlet and exit flow angles to rotor are tan ₁ R+(4/2) and R-(4/2) tan ß₂ = R d. Calculate inlet and exit flow angles of the relative velocity to the rotor e. Calculate inlet flow angle to stator