Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Senad Iseni"'
Autor:
Senad Iseni, Mahesh R. G. Prasad, Niels Modeler, Alexander Hartmaier, Klaudiusz Holeczek, Francesca di Mare
Publikováno v:
Volume 10A: Structures and Dynamics.
A major technical challenge for modern aero engines is the development of designs which reduce noise and emission whilst increasing aerodynamic efficiency and ensuring aeroelastic stability of low-temperature engine components such as fans and low-pr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::260798f98d63e7cf03fd468c3a1fa23f
https://doi.org/10.1115/gt2020-14951
https://doi.org/10.1115/gt2020-14951
Publikováno v:
CEAS Aeronautical Journal. 10:805-815
This paper describes a detailed flutter analysis of fan casing contour modifications on a scaled high-speed fan to investigate the influence and effect on flutter boundaries. The flutter analysis focusses on discrete selected members from a previous
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cd257299bbe445916f37409c5d8b92ce
https://doi.org/10.1007/s13272-018-0351-y
https://doi.org/10.1007/s13272-018-0351-y
Autor:
Tim Sauer, Dieter Peitsch, Antoine Moreau, Ronald Mailach, Senad Iseni, Derek Micallef, Eberhard Nicke, Anne-Laure Aulich, Lars Enghardt
Publikováno v:
CEAS Aeronautical Journal. 8:157-166
Aircraft propulsion will continue to rely on gas turbine technology for the next decades to come. Thus, to achieve environmental agreements, ensure engine safety, and retain economic competitiveness, ongoing development with a multidisciplinary desig
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b64acbc40c42d6704a1a5e0fae4fe04a
https://doi.org/10.1007/s13272-016-0226-z
https://doi.org/10.1007/s13272-016-0226-z
Autor:
Francesca di Mare, Derek Micallef, Ronald Mailach, Matthias Kniefs, Martin Lange, Senad Iseni
Publikováno v:
Volume 7C: Structures and Dynamics.
Circumferential grooves in the casing of an axial compressor rotor or fan are known to be beneficial by extending the operating range of the machine. The goal of this paper is to analyze, if such grooves have a significant effect on the flutter stabi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::471a772668c84de7bdee34db1550d85d
https://doi.org/10.1115/gt2018-76422
https://doi.org/10.1115/gt2018-76422
Publikováno v:
Volume 7B: Structures and Dynamics.
The fundamental mechanisms of blade flutter in modern aircraft engines are very complex. Flutter is a self-excited aeroelastic instability phenomenon which can finally cause material fatigue and, in the worst case, leads to blade failure within a ver
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::66aad18cb65b77ba6df004989c686f5a
https://doi.org/10.1115/gt2016-56593
https://doi.org/10.1115/gt2016-56593
Autor:
Omer Hodzic, Martin Sinkwitz, Andreas Schramm, Senad Iseni, David Engelmann, Di Mare, Francesca, Mailach, Ronald, International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (17. : 2017 : Maui)
Publikováno v:
Ruhr-Universität Bochum
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::026b726793912eadd473e3e41b6855db
http://isromac-isimet.univ-lille1.fr/upload_dir/finalpaper17/93.finalpaper.pdf
http://isromac-isimet.univ-lille1.fr/upload_dir/finalpaper17/93.finalpaper.pdf
