Hauke Müller
Current Organizations / Institutes
The organizations/institutes from the scholar's latest article
Research Subjects
Research Interests
Hauke Müller has a total of 6 co-authors. Here are the top co-authors by number of shared publications:
- Alexandra Schneider
Institute of Gas Turbines and Aerospace Propulsion, Technical University of Darmstadt, Otto-Berndt-Straße 2, 64287 Darmstadt, Germany
1 shared publication - Bernd Becker
Rolls-Royce Deutschland Ltd. & Co. KG, Eschenweg 11, 15827 Blankenfelde-Mahlow, Germany
1 shared publication - Daniel Franke
Technical University of Darmstadt, Institute of Gas Turbines and Aerospace Propulsion, Otto-Bernd-Straße 2, 64287 Darmstadt, Germany
1 shared publication - Fabian Klausmann
Institute of Gas Turbines and Aerospace Propulsion, Technical University of Darmstadt, Otto-Berndt-Straße 2, 64287 Darmstadt, Germany
1 shared publication - Heinz-Peter Schiffer
Institute of Gas Turbines and Aerospace Propulsion, Technical University of Darmstadt, Otto-Berndt-Straße 2, 64287 Darmstadt, Germany
1 shared publication - Jonas Foret
Institute of Gas Turbines and Aerospace Propulsion, Technical University of Darmstadt, Otto-Berndt-Straße 2, 64287 Darmstadt, Germany
1 shared publication
Latest Publications
- Open Access
- 22 June 2021
- Published by MDPI AG in International Journal of Turbomachinery, Propulsion and Power
- Vol. 6 (3) , 21
Experimental Aerodynamic and Aeroelastic Investigation of a Highly-Loaded 1.5-Stage Transonic Compressor with Tandem Stator
This paper experimentally investigates a highly-loaded 1.5-stage transonic axial compressor, which comprises a variable inlet guide vane, a BLISK rotor, and a variable stator in tandem arrangement. A detailed comparison between the newly designed compressor stage and a reference stage with a conventional stator design was conducted by using extensive instrumentation. Thus, steady and unsteady phenomena—focusing on the aerodynamic and aeroelastic behavior—were analyzed. Due to the new stator vane design, a higher aerodynamic stator vane loading was pursued, while the vane count was reduced. This, in turn, allowed a rotor design with an increased work coefficient. This experimental study revealed several effects of the optimized compressor stage in terms of both performance and the corresponding aerodynamics, as well as the aeroelastic behavior.
- 22 June 2021
- Published by MDPI AG in International Journal of Turbomachinery, Propulsion and Power
- Vol. 6 (3) , 21
Open AccessExperimental Aerodynamic and Aeroelastic Investigation of a Highly-Loaded 1.5-Stage Transonic Compressor with Tandem Stator
This paper experimentally investigates a highly-loaded 1.5-stage transonic axial compressor, which comprises a variable inlet guide vane, a BLISK rotor, and a variable stator in tandem arrangement. A detailed comparison between the newly designed compressor stage and a reference stage with a conventional stator design was conducted by using extensive instrumentation. Thus, steady and unsteady phenomena—focusing on the aerodynamic and aeroelastic behavior—were analyzed. Due to the new stator vane design, a higher aerodynamic stator vane loading was pursued, while the vane count was reduced. This, in turn, allowed a rotor design with an increased work coefficient. This experimental study revealed several effects of the optimized compressor stage in terms of both performance and the corresponding aerodynamics, as well as the aeroelastic behavior.