Basic Principles
Published in Cambridge University Press eBooks • Feb 17, 2011
Authors:
Christopher E. Brennen
Abstract
The geometry of a generalized turbomachine rotor is sketched in figure 2.1, and consists of a set of rotor blades (number = ZR) attached to a hub and operating within a static casing. The radii of the inlet blade tip, inlet blade hub, discharge blade tip, and discharge blade hub are denoted by RT1, ...
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