Gründler, Jonathan ; Lehmann, Knut ; Schiffer, Heinz-Peter (2024)
The Effect of Unsteady Inlet Boundary Conditions on the Aero-Thermal Behavior of High-Pressure Turbine Vanes – A Numerical Study Using Scale-Resolving Simulations.
In: Journal of Turbomachinery, 147 (1)
doi: 10.1115/1.4065858
Artikel, Bibliographie

Gründler, Jonathan ; Lehmann, Knut ; Schiffer, Heinz-Peter (2023)
The Effect of Unsteady Inlet Boundary Conditions on the Aero-Thermal Behavior of High-Pressure Turbine Vanes: A Numerical Study Using Scale-Resolving Simulations.
ASME Turbo Expo 2023: Turbomachinery Technical Conference and Exposition. Boston, Massachusetts, USA (26.06.2023-30.06.2023)
doi: 10.1115/GT2023-100884
Konferenzveröffentlichung, Bibliographie

Gründler, Jonathan ; Schiffer, Heinz-Peter ; Lehmann, Knut (2022)
An Efficient Unsteady 1-Way Coupling Method of Combustor and Turbine.
Turbo Expo 2022: Turbomachinery Technical Conference and Exposition. Rotterdam (13.06.2022-17.06.2022)
doi: 10.1115/GT2022-78056
Konferenzveröffentlichung, Bibliographie

Schneider, Marius ; Lehmann, Knut ; Schiffer, Heinz-Peter (2017)
Parameterised Model of 2D Combustor Exit Flow Conditions for High Pressure Turbine Simulations.
12th European Turbomachinery Conference. Stockholm, Sweden (03.04.2017-07.04.2017)
Konferenzveröffentlichung, Bibliographie

Schneider, Marius ; Lehmann, Knut ; Schiffer, Heinz-Peter (2017)
Parameterised Model of 2D Combustor Exit Flow Conditions for High-Pressure Turbine Simulations.
In: International Journal of Turbomachinery, Propulsion and Power, 2 (4)
doi: 10.3390/ijtpp2040020
Artikel, Bibliographie

Werschnik, Holger ; Krichbaum, Alexander ; Lehmann, Knut ; Schiffer, Heinz-Peter (2015)
The Influence of Combustor Swirl on Turbine Stator Endwall Heat Transfer and Film Cooling Effectiveness in a 1.5-Stage Axial Turbine.
Proceedings of the 22nd ISABE, Phoenix/USA, Paper No. 2015-20184.
Konferenzveröffentlichung, Bibliographie

Krichbaum, Alexander ; Werschnik, Holger ; Wilhelm, Manuel ; Lehmann, Knut ; Schiffer, Heinz-Peter (2015)
A Large Scale Turbine Test Rig for the Investigation of High Pressure Turbine Aerodynamics and Heat Transfer with Variable Inflow Conditions: GT2015-43261.
Proceedings of ASME Turbo Expo 2015, Montréal, Canada.
Konferenzveröffentlichung, Bibliographie