Predicted Transient Performance of a Derivative Two-Spool Turbofan Engine With a 4-Stage I.P. Compressor

Darbouche, Lamine Mohamed (1991) Predicted Transient Performance of a Derivative Two-Spool Turbofan Engine With a 4-Stage I.P. Compressor. MSc(R) thesis, University of Glasgow.

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Abstract

Given the need of a higher thrust, with a higher overall efficiency engine for civil aircraft, a method of designing a derivative engine from an existing engine is investigated in the present work.

Item Type: Thesis (MSc(R))
Qualification Level: Masters
Keywords: Mechanical engineering
Date of Award: 1991
Depositing User: Enlighten Team
Unique ID: glathesis:1991-77065
Copyright: Copyright of this thesis is held by the author.
Date Deposited: 14 Jan 2020 09:21
Last Modified: 14 Jan 2020 09:21
URI: http://theses.gla.ac.uk/id/eprint/77065

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