Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Matthias Schleer"'
Autor:
Matthias Schleer, B. Ribi, S. S. Hong, Christian Roduner, F. Pløger, Mehrdad Zangeneh, Reza S. Abhari
Publikováno v:
Journal of Turbomachinery. 126:82-90
This paper presents an experimental investigation of two centrifugal compressor stage configurations. The baseline configuration has been designed using conventional design engineering tools. The second configuration was designed using advanced inver
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ac61c58f021f0e0dc578b9e0d3cd3e8b
https://doi.org/10.1115/1.1625690
https://doi.org/10.1115/1.1625690
Autor:
Matthias Schleer, B. Ribi, Mehrdad Zangeneh, F. Pløger, Reza S. Abhari, S. S. Hong, Christian Roduner
Publikováno v:
Journal of Turbomachinery. 126:73-81
In this paper the three-dimensional inverse design code TURBOdesign-1 is applied to the design of the blade geometry of a centrifugal compressor impeller with splitter blades. In the design of conventional impellers the splitter blades normally have
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::658b3b7793e52c8666423affc4dfca26
https://doi.org/10.1115/1.1645868
https://doi.org/10.1115/1.1645868
Publikováno v:
Volume 6: Structures and Dynamics, Parts A and B.
As the second part of a two-part paper, this paper presents an experimental investigation of forced response impeller blade vibrations in a centrifugal compressor stage caused by variable inlet guide vanes. Although it is common practice to experimen
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::54fc4a5fdb9d22f6808843169f2c96a4
https://doi.org/10.1115/gt2011-46290
https://doi.org/10.1115/gt2011-46290
Publikováno v:
Volume 7: Turbomachinery, Parts A, B, and C.
The aim of the current paper is to investigate the evolution of the flow in the vaneless diffuser of a scaled-up turbocharger compressor using the steady-state viscous calculations. First, the predicted flow patterns are compared with the detailed la
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a615e266114cf1c4f9b56c6d03d55229
https://doi.org/10.1115/gt2010-22605
https://doi.org/10.1115/gt2010-22605
Autor:
Matthias Schleer, Reza S. Abhari
Publikováno v:
Volume 6: Turbomachinery, Parts A and B.
This work reports on flow measurements taken within the vaneless diffuser of an scaled-up model of a small-scale, highly loaded unshrouded compressor with large relative tip clearance. The aims are to describe and to analyze the influence of the clea
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7d89eaf833ddede625deba5e4a70fe63
https://doi.org/10.1115/gt2006-90083
https://doi.org/10.1115/gt2006-90083
Publikováno v:
Volume 6: Turbomachinery, Parts A and B.
This report intends to shed an insight into the effect of large relative tip clearances on the onset of instability in a highly loaded centrifugal compressor. Time-resolved pressure measurements have been performed along the casing of a scaled-up mod
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::709b090ae9a850c30e3bb6328087d35d
https://doi.org/10.1115/gt2006-90084
https://doi.org/10.1115/gt2006-90084
Autor:
Reza S. Abhari, Matthias Schleer
Publikováno v:
Volume 6: Turbo Expo 2005, Parts A and B.
In this work the stability behavior of small-scale centrifugal compressor is evaluated in detail and the influence of design features typical for small-scale applications is shown. The impeller used in this study represents the design features of mac
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3c8f911a2f51c5c033047ebdc030eea1
https://doi.org/10.1115/gt2005-68713
https://doi.org/10.1115/gt2005-68713
Publikováno v:
Volume 6: Turbo Expo 2003, Parts A and B.
This paper reports on the results of experimental work using LDA in the flow path of a centrifugal compressor with a vaned diffuser. The work was done in the ‘RIGI’ facility in the Turbomachinery Laboratory (‘LSM’) of ETH Zurich. The flow-fie
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3113604a9c806a9cb7e1c4f8f3cb7629
https://doi.org/10.1115/gt2003-38476
https://doi.org/10.1115/gt2003-38476
Publikováno v:
Volume 2: Symposia, Parts A, B, and C.
To see the tip clearance effect on a centrifugal compressor, time-resolved flow measurements were carried out at the discharge of a centrifugal compressor impeller, which is 30 deg back swept from radial and operated at the blade tip speed of 260 m/s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dcbd8f56054eb146c6f21666ebf43806
https://doi.org/10.1115/fedsm2003-45094
https://doi.org/10.1115/fedsm2003-45094