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Design of the Compression System of a Geared Turbofan

Immery, Thomas (2018) Design of the Compression System of a Geared Turbofan. Diploma, ENSIAME (École nationale supérieure d'ingénieurs en informatique, automatique, mécanique, énergétique et électronique).

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Item URL in elib:https://elib.dlr.de/122567/
Document Type:Thesis (Diploma)
Title:Design of the Compression System of a Geared Turbofan
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Immery, ThomasUNSPECIFIEDUNSPECIFIED
Date:October 2018
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:50
Status:Published
Keywords:Compressor, Design, Geared Turbofan, Throughflow
Institution:ENSIAME (École nationale supérieure d'ingénieurs en informatique, automatique, mécanique, énergétique et électronique)
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:propulsion systems
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Fan and Compressor Technologies (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Fan and Compressor
Deposited By: Schnös, Markus
Deposited On:06 Nov 2018 09:18
Last Modified:06 Nov 2018 09:18

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