This thesis is part of a more extensive work of research focused on the study of turboshaft engines for helicopter applications.The purpose of this work is to design a GE-T700-based free power axial-flow turbine model which serves as a baseline for future developments.The preliminary design was performed implementing an iterative calculation procedure, then the model developed from the calculation output data was verified by means of Computational Fluid Dynamics (CFD)
Design and CFD analysis of an axial-flow gas turbine
Grandi, Giada
2014/2015
Abstract
This thesis is part of a more extensive work of research focused on the study of turboshaft engines for helicopter applications.The purpose of this work is to design a GE-T700-based free power axial-flow turbine model which serves as a baseline for future developments.The preliminary design was performed implementing an iterative calculation procedure, then the model developed from the calculation output data was verified by means of Computational Fluid Dynamics (CFD)File in questo prodotto:
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TESI_GRANDI_GIADA_1039538.pdf
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Utilizza questo identificativo per citare o creare un link a questo documento:
https://hdl.handle.net/20.500.12608/19153