1.

Flow coefficient in axial compressor is defined as-______. (Axial velocity of flow = vf, Blade velocity at periphery = u)

A. \(\frac{{{v_f}}}{u}\)
B. \(\frac{u}{{{v_f}}}\)
C. \(\frac{{{v_f} + u}}{u}\)
D. \(\frac{{{u^2}}}{{{v_f}}}\)
Answer» B. \(\frac{u}{{{v_f}}}\)


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