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The air flow passages between adjacent axial compressor rotor blades in a gas turbine engine are divergent. However, the exit velocity is higher than the
The air flow passages between adjacent axial compressor rotor blades in a gas turbine engine are divergent. However, the exit velocity is higher than the entry velocity of the rotor. The reason for this is
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Fundamentals of Thermodynamics
Authors: Richard E. Sonntag, Claus Borgnakke, Gordon J. Van Wylen
6th edition
471152323, 978-0471152323
