Abstract
In Chapter 6, we derived the equations for calculation of different losses that occur within a stage of a turbomachine. As shown, the sum of those losses determines the stage efficiency which shows the capability of energy conversion within the stage. The stage efficiency, however, is not fully identical with the efficiency of the entire turbomachine.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
Bibliography
Traupel, W., Thermische Turbomaschinen, Bd.I, 1977, Springer-Verlag Berlin Heidelberg New York.
Vavra, M. H., 1960, Aero-Thermodynamics and Flow in Turbomachines, John Wiley & Sons, Inc.
Author information
Authors and Affiliations
Corresponding author
Rights and permissions
Copyright information
© 2019 Springer Nature Switzerland AG
About this chapter
Cite this chapter
Schobeiri, M.T. (2019). Efficiency of Multi-Stage Turbomachines. In: Gas Turbine Design, Components and System Design Integration. Springer, Cham. https://doi.org/10.1007/978-3-030-23973-2_7
Download citation
DOI: https://doi.org/10.1007/978-3-030-23973-2_7
Published:
Publisher Name: Springer, Cham
Print ISBN: 978-3-030-23972-5
Online ISBN: 978-3-030-23973-2
eBook Packages: Physics and AstronomyPhysics and Astronomy (R0)