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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