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.

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: https://theses.gla.ac.uk/id/eprint/77065