Combustion gas turbine for airplanes

Combustion gas turbine for airplanes

This paper contains a theoretical study of various thermodynamic cycles for Gas-Turbine-propeller propulsion units for aircraft. The object of the study was to evaluate the turbine-propeller engines as a source of power for fast, economical, long range airplanes. Hence, the consumption of fuel an...

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Bibliographic Details
Main Author: Lancaster, Otis Ewing
Format: Others
Published: 1945
Online Access:https://thesis.library.caltech.edu/4654/1/Lancaster_oe_1945.pdf
Lancaster, Otis Ewing (1945) Combustion gas turbine for airplanes. Engineer's thesis, California Institute of Technology. doi:10.7907/82FF-C054. https://resolver.caltech.edu/CaltechETD:etd-11242008-110400 <https://resolver.caltech.edu/CaltechETD:etd-11242008-110400>

Internet

https://thesis.library.caltech.edu/4654/1/Lancaster_oe_1945.pdf
Lancaster, Otis Ewing (1945) Combustion gas turbine for airplanes. Engineer's thesis, California Institute of Technology. doi:10.7907/82FF-C054. https://resolver.caltech.edu/CaltechETD:etd-11242008-110400 <https://resolver.caltech.edu/CaltechETD:etd-11242008-110400>

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