Untersuchung zur Evaluierung von Forschungspotentialen hinsichtlich Prozessen, Komponenten und Werkstoffen von trans- und superkritischen CO2-Anwendungen. Stuttgart, 2016. [PUMA: unibibliografie ubs_10004 ubs_40074 ubs_40071 ubs_30046 ubs_30047 liste ubs_20004 mult ubs_30050 ubs_40284] URL
Second Law Analysis of Condensing Steam Flows. Journal of engineering for gas turbines and power, (140)12:121003, ASME, 2018. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
Second law analysis of condensing steam flows. Proceedings of the ASME Turbo Expo: Turbomachinery Technical Conference and Exposition - 2018, (8):V008T29A025, American Society of Mechanical Engineers, New York, NY, 2018. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
Results of the International Wet Steam Modeling Project. Proceedings of the Institution of Mechanical Engineers. Part A, Journal of Power and Energy, 232, 5:550-570, Sage Publ., London, 2018. [PUMA: unibibliografie ubs_10004 oa ubs_20004 wos ubs_30050 ubs_40284]
Reducing Blade Force Response in a Radial Turbine by Means of Jet Injection. Proceedings of the ASME Turbo Expo : Turbomachinery Technical Conference and Exposition - 2019, (7, A : Emerging Methods in Design and Engineering; Fatigue, Fracture, and Life Prediction; Probabilistic Methods; Rotordynamics; Aerodynamic Excitation and Damping):V07AT36A007, The American Society of Mechanical Engineers, New York, N.Y., 2019. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
Prediction of Transient Pressure Fluctuations within a Low-Pressure Turbine Cascade Using a Lanczos-Filtered Harmonic Balance Method. International journal of turbomachinery, propulsion and power, (6)3:25, MDPI, 2021. [PUMA: unibibliografie ubs_10004 oa ubs_20004 wos ubs_30050 ubs_40284]
Prediction of Low-Engine-Order Excitation Due to a Nonsymmetrical NozzleRing in a Radial Turbine by Means of the Nonlinear Harmonic Approach. Journal of Engineering for Gas Turbines and Power, (141)12:121004, ASME, 2019. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
Prediction of Low-Engine-Order Excitation Due to a Nonsymmetrical Nozzle Ring in a Radial Turbine by Means of the Nonlinear Harmonic Approach. Proceedings of the ASME Turbo Expo : Turbomachinery Technical Conference and Exposition - 2019, (7, A : Emerging Methods in Design and Engineering; Fatigue, Fracture, and Life Prediction; Probabilistic Methods; Rotordynamics; Aerodynamic Excitation and Damping):V07AT36A003, The American Society of Mechanical Engineers, New York, N.Y., 2019. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
Prediction of Aerodynamically Induced Blade Vibrations in a Radial Turbine Rotor Using the Nonlinear Harmonic Approach. Journal of Engineering for Gas Turbines and Power, (141)2:021007, ASME, 2019. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
Prediction of Aerodynamically Induced Blade Vibrations in a Radial Turbine Rotor Using the Nonlinear Harmonic Approach. Proceedings of the ASME Turbo Expo : Turbomachinery Technical Conference and Exposition, (7C : Structures and Dynamics):GT2018-76814, V07CT36A020, ASME, 2018. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
On the Influence of Blade Aspect Ratio on Aerodynamic Damping. Journal Of Turbomachinery, 141, 10:101007, ASME, New York, 2019. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
On the far-field boundary condition treatment in the framework of aeromechanical computations using ANSYS CFX. Proceedings of the Institution of Mechanical Engineers. Part A, Journal of power and energy, (235)5:1103-1118, Sage Publications, 2021. [PUMA: unibibliografie ubs_10004 oa ubs_20004 wos ubs_30050 ubs_40284]
Numerical investigations of an axial exhaust diffuser coupling the last stage of a generic gas turbine. Journal of engineering for gas turbines and power, (141)3:031025, ASME, 2019. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
Numerical Investigations of an Axial Exhaust Diffuser Coupling the Last Stage of a Generic Gas Turbine. Proceedings of the ASME Turbo Expo : Turbomachinery Technical Conference and Exposition, (2B : Turbomachinery):V02BT43A003, ASME, 2018. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
Numerical Investigation Of The Influence Of Hood Height Variation On Performance Of Low Pressure Steam Turbine Exhaust Hoods. Proceedings of the ASME Turbo Expo : Turbomachinery Technical Conference and Exposition, (8 : Microturbines, Turbochargers, and Small Turbomachines; Steam Turbines):GT2018-76562, V008T29A031, ASME, 2018. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
Numerical Investigation of the Influence of Flow Deflection at the Upper Hood on Performance of Low Pressure Steam Turbine Exhaust Hoods. Proceedings of the ASME Turbo Expo : Turbomachinery Technical Conference and Exposition - 2019, (8 : Microturbines, turbochargers, and small turbomachines; steam turbines):V008T29A008, The American Society of Mechanical Engineers, New York, N.Y., 2019. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
Numerical Investigation of Boundary Layers in Wet Steam Nozzles. Journal of engineering for gas turbines and power, (139)1:012606, ASME, 2017. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
Multi-Objective Numerical Optimization of Radial Turbines. Journal of turbomachinery, (146)3:031004, American Society of Mechanical Engineers, 2024. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
Modelling of condensing steam flows in Laval nozzles with ANSYS CFX. In Ondřej Bartoš, and Michal Kolovratník (Eds.), Special Issue: Wet Steam 2016, 232, 5, SI:571-575, Sage Publications, 2018. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
Mistuning and Damping of a Radial Turbine Wheel : Part 1: Fundamental Analyses and Design of Intentional Mistuning Pattern. Journal of engineering for gas turbines and power, (144)2:021012, American Society of Mechanical Engineers, 2022. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
Investigation of the Impact of Unsteady Turbulence Effects on the Aeroelastic Analysis of a Low-Pressure Turbine Rotor Blade. Journal of Turbomachinery, 141, 10:100801, ASME, New York, 2019. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
Investigation of the Flow Field and the Pressure Recovery in a Gas Turbine Exhaust Diffuser at Design, Part-Load, and Over-Load Conditions. Journal of turbomachinery, (144)8:081010, American Society of Mechanical Engineers, 2022. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
Influence of Turbocharger Turbine Blade Geometry on Vibratory Blade Stresses. Proceedings Of The ASME Turbo Expo : Turbomachinery Technical Conference And Exposition, (2D : Turbomachinery):GT2018-76226, V02DT46A014, ASME, 2018. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
Influence of turbocharger turbine blade geometry on vibratory blade stresses. Journal of Engineering for Gas Turbines and Power-Transactions of the ASME, (141)2:021015, ASME, 2019. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
Influence of Tip Shroud Modeling on the Flutter Stability of a Low Pressure Turbine Rotor. Proceedings of the ASME Turbo Expo : Turbomachinery Technical Conference and Exposition - 2019, (7, A : Emerging Methods in Design and Engineering; Fatigue, Fracture, and Life Prediction; Probabilistic Methods; Rotordynamics; Aerodynamic Excitation and Damping):V07AT36A012, The American Society of Mechanical Engineers, New York, N.Y., 2019. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
Forced Response Analysis of a Mistuned, Compressor Blisk Comparing Three Different Reduced Order Model Approaches. Journal of engineering for gas turbines and power, (139)6:062501, ASME, 2017. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
Forced Response Analysis of a Mistuned Blisk Using Noncyclic Reduced-Order Models. Journal of Propulsion and Power, (34)3:565-577, AIAA, 2018. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
Experimental evaluation of heat transfer effect on turbocompressor performance operating with helium-neon gas mixtures. EPJ Techniques and Instrumentation, (9):6, Springer, 2022. [PUMA: unibibliografie ubs_10004 oa dfg ubs_20004 f2022 oafonds ubs_30050 ubs_40284]
Experimental and Numerical Similitude Study Using a Novel Turbocompressor Test Facility Operating With Helium-Neon Gas Mixtures. Journal of turbomachinery, (144)8:081015, American Society of Mechanical Engineers, 2022. [PUMA: unibibliografie ubs_10004 oa ubs_20004 wos ubs_30050 ubs_40284]
Experimental and Numerical Assessment of the Impact of Part-Span Connectors on Turbine Efficiency and Flow Field. Proceedings of the ASME Turbo Expo : Turbomachinery Technical Conference and Exposition - 2019, (8 : Microturbines, turbochargers, and small turbomachines; steam turbines):V008T29A030, The American Society of Mechanical Engineers, New York, N.Y., 2019. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
Detached-Eddy Simulation Applied to the Tip-Clearance Flow in a Last Stage Steam Turbine Blade. Proceedings of the ASME Turbo Expo : Turbomachinery Technical Conference and Exposition, (8 : Microturbines, Turbochargers, and Small Turbomachines; Steam Turbines):GT2018-75943, V008T29A020, ASME, 2018. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
Detached-Eddy Simulation Applied to Aeroelastic Stability Analysis in a Last-Stage Steam Turbine Blade. Journal of Turbomachinery, (141)9:091002, ASME, 2019. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
Blade Vibration Analysis for Radial Turbine Featuring a Multi-Channel Casing Design. Journal of turbomachinery, (145)8:081003, American Society of Mechanical Engineers, 2023. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
Assessment of Low Engine Order Excitation of a Contaminated Turbocharger Radial Turbine Stage Using a Nozzle Ring Only Computational Model. Journal of turbomachinery, (145)1:011011, American Society of Mechanical Engineers, 2023. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
An Extension of the Classical Subset of Nominal Modes Method for the Model Order Reduction of Gyroscopic Systems. Journal of Engineering for Gas Turbines and Power-Transactions of the ASME, (141)5:052501, ASME, 2019. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
An Extension of the Classical Subset of Nominal Modes Method for the Model Order Reduction of Gyroscopic Systems. ASME Turbo Expo 2018 : Turbomachinery Technical Conference And Exposition, (7C : Structures and Dynamics)ASME, New York, NY, 2018. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
An empirical approach to predict droplet impact erosion in low-pressure stages of steam turbines. Wear, (402):57-63, Elsevier Science SA, 2018. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
Aerodynamic Excitation Analysis of a Radial Turbine Featuring a Multi-Channel Casing Design. Proceedings of the ASME Turbo Expo : Turbomachinery Technical Conference and Exposition - 2019, (7, A : Emerging Methods in Design And Engineering; Fatigue, Fracture, and Life Prediction; Probabilistic Methods; Rotordynamics; Aerodynamic Excitation and Damping):V07AT36A001, The American Society of Mechanical Engineers, New York, N.Y., 2019. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
Aeroacoustic Analysis of Low-Speed Axial Fans With Different Rotational Speeds in the Design Point. Journal of engineering for gas turbines and power, (140)5:052601, ASME, 2018. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
A New Mistuning Identification Method Based on the Subset of Nominal System Modes Method. Journal of Engineering for Gas Turbines and Power, (142)2:021016, The American Society of Mechanical Engineers, 2020. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
A generic low-pressure steam turbine test case for aeromechanics and condensation. Proceedings of the Institution of Mechanical Engineers. Part A, Journal of Power and Energy, (233)7:953-958, Sage Publ., 2019. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]
A Consistent and Implicit Rhie-Chow Interpolation for Drag Forces in Coupled Multiphase Solvers. International journal of turbomachinery, propulsion and power, (6)2:7, MDPI, 2021. [PUMA: unibibliografie ubs_10004 oa ubs_20004 wos ubs_30050 ubs_40284]
A Comparison of Two Reduced Order Methods for Probabilistic Mistuning Investigations. ASME 2017 Gas Turbine India Conference, 2The American Society of Mechanical Engineers, New York, NY, 2018. [PUMA: unibibliografie ubs_10004 ubs_20004 wos ubs_30050 ubs_40284]