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Numeric Investigation of a Compressor cascade with smooth and rough walls

Massias, E. (2003) Numeric Investigation of a Compressor cascade with smooth and rough walls. Diploma. DLR-Interner Bericht. IB-325-01-03, 62 S.

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Item URL in elib:https://elib.dlr.de/44476/
Document Type:Monograph (DLR-Interner Bericht, Diploma)
Title:Numeric Investigation of a Compressor cascade with smooth and rough walls
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Massias, E.UNSPECIFIEDUNSPECIFIED
Date:January 2003
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:62
Status:Published
Keywords:Transonic compressor, blading design,
Institution:ENSIAME - Valenciennes
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Propulsion Systems (old)
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: Fox, Rosemarie
Deposited On:18 Aug 2006
Last Modified:27 Apr 2009 13:01

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