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MCS,PHD
Argosy University/ Phoniex University/
Nov-2005 - Oct-2011
Professor
Phoniex University
Oct-2001 - Nov-2016
Sketched in Fig. P12.10 are the upstream [section (1)] and downstream [section (2)] velocity triangles at the arithmetic mean radius for flow through an axial-flow turbomachine rotor. The axial component of velocity is 50 ft/s at sections (1) and (2).
(a) Label each velocity vector appropriately. Use V for absolute velocity, W for relative velocity, and U for blade velocity.
(b) Are you dealing with a turbine or a fan?
(c) Calculate the work per unit mass involved.
(d) Sketch a reasonable blade section. Do you think that the actual blade exit angle will need to be less or greater than 15°? Why?

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