Zobrazeno 1 - 10
of 17
pro vyhledávání: '"Dominik Broszat"'
Publikováno v:
2018 AIAA/CEAS Aeroacoustics Conference.
Autor:
Franz Heitmeir, Sabine Bauinger, Loris Simonassi, Dominik Broszat, Manuel Zenz, Florian Schönleitner, Andreas Marn
Publikováno v:
European Conference on Turbomachinery Fluid Dynamics and hermodynamics.
This work presents results from experimental investigations conducted in the subsonic test turbine facility for aerodynamic, acoustic, and aeroelastic investigations at Graz University of Technology. The experiments have been performed for the acoust
Autor:
Franz Heitmeir, Andreas Marn, Martin Hoeger, Florian Schönleitner, Dominik Broszat, Thorsten Selic
Publikováno v:
Journal of Energy and Power Engineering. 10
Autor:
Franz Heitmeir, Martin Hoeger, Florian Schönleitner, Thorsten Selic, Andreas Marn, Dominik Broszat, Stefan Zerobin
Publikováno v:
21st AIAA/CEAS Aeroacoustics Conference.
In this paper the sound power levels of three different designs of turbine exit guide vanes (TEGV) of turbine exit casings are compared with a standard design of an TEGV. The comparison is made with respect to the LPT for the acoustically relevant op
Autor:
Franz Heitmeir, Dominik Broszat, Martin Hoeger, Andreas Marn, Florian Schönleitner, Thorsten Selic
Publikováno v:
21st AIAA/CEAS Aeroacoustics Conference.
In a number of publications of the past years, the authors have presented detailed descriptions of the STTF acoustic turbine test facility at the Graz University of Technology and highlighted its importance for tool validation and technology verifica
Publikováno v:
Journal of Turbomachinery. 137
Within previous EU projects, possible modifications to the engine architecture have been investigated, which would allow for an optimized aerodynamic or acoustic design of the exit guide vanes (EGVs) of the turbine exit casing (TEC). However, the eng
Publikováno v:
Volume 2C: Turbomachinery.
This paper presents measurement results of a 1½ stage LPT test rig at Graz University of Technology incorporating two different rotor geometries: one with a regular blade loading and a second rotor with a highly loaded blade geometry. The test rig w
Publikováno v:
Volume 2A: Turbomachinery.
Within previous EU projects, possible modifications to the engine architecture have been investigated, that would allow for an optimised aerodynamic or acoustic design of the exit guide vanes (EGV) of the turbine exit casing (TEC). However, the engin
Autor:
Emil Göttlich, Mirko Spitalny, Dominik Broszat, Andreas Marn, Stefan Zerobin, Christian Faustmann
Publikováno v:
20th AIAA/CEAS Aeroacoustics Conference.
The paper deals with the investigation on the acoustics of two different turning mid turbine frames (TMTF) in the two-stage two-spool test turbine located at the Institute for Thermal Turbomachinery and Machine Dynamics (ITTM) of Graz University of T
Publikováno v:
19th AIAA/CEAS Aeroacoustics Conference.
Within the scope of the author’s previous papers, the general setup of an acoustic turbine test facility at the Graz University of Technology has been presented. In addition, its significance for the validation of acoustic prediction tools and the