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Erschienen in:

2021 | OriginalPaper | Buchkapitel

3. Preliminary Design of Axial Flow Turbines

verfasst von : Marco Gambini, Michela Vellini

Erschienen in: Turbomachinery

Verlag: Springer International Publishing

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Abstract

With reference to an axial turbine stage, a procedure for the calculation of kinematic parameters at mean diameter (Sect. 3.1), thermodynamic parameters (Sect. 3.2), geometric parameters (Sect. 3.3), parameters in the radial direction (Sect. 3.4) and stage losses (Sect. 3.5) is provided. Then, Sect. 3.6 discusses the input parameters of this procedure and suggests their numerical values to be used in the calculations. Finally, Sect. 3.7 illustrates the procedure for extending calculations to multistage turbines. The numerical application of the proposed procedure, aimed at the preliminary design of multistage axial turbines, is instead developed in Chap. 8.

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Vorheriges Kapitel Turbomachinery Selection

Nächstes Kapitel Preliminary Design of Axial Flow Compressors

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Titel: Preliminary Design of Axial Flow Turbines
verfasst von: Marco Gambini
Michela Vellini
Verlag: Springer International Publishing
Buch: Turbomachinery
Print ISBN: 978-3-030-51298-9

Electronic ISBN: 978-3-030-51299-6

Copyright-Jahr: 2021
DOI: https://doi.org/10.1007/978-3-030-51299-6_3

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