Login
Document type:
Konferenzbeitrag / Conference Paper
Title:
Influence of Tip Clearance, Aspect Ratio, Blade Loading and Inlet Boundary Layer on Secondary Losses in Compressor Cascades
Title of conference publication:
ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition
Subtitle of conference publication:
Volume 1: Turbomachinery: Birmingham, UK, June 10–13, 1996
Conference title:
ASME Turbo Expo (1996, Birmingham)
Venue:
Birmingham
Year of conference:
1996
Date of conference beginning:
10.06.1996
Date of conference ending:
13.06.1996
Publishing institution:
ASME
Year:
1996
Language:
Englisch
ISBN:
978-0-7918-7872-9
Article ID:
96-GT-505
DOI:
Department:
Fakultät für Luft- und Raumfahrttechnik
Institute:
LRT 12 - Institut für Strahlantriebe
Chair:
Niehuis, Reinhard; Fottner, Leonhard
Open Access yes or no?:
Ja / Yes
BibTeX