1-11 of 11
Robin Schmidt
Close
Save search
Follow your search
Access your saved searches in your account
Would you like to receive an alert when new items match your search?
Close Modal
Sort by
Proceedings Papers

Robust Optimization of a Compressor Blade Through Combination of an Adjoint-Based Multistart Approach and Global Gaussian Process Regression

Aryan Karimian, Robin Schmidt, Christian Janke
Proc. ASME. GT2024, Volume 12D: Turbomachinery — Multidisciplinary Design Approaches, Optimization, and Uncertainty Quantification; Radial Turbomachinery Aerodynamics; Unsteady Flows in Turbomachinery, V12DT34A002, June 24–28, 2024
Publisher: American Society of Mechanical Engineers
Paper No: GT2024-121351
https://doi.org/10.1115/GT2024-121351
View Paper titled, Robust Optimization of a Compressor Blade Through Combination of an Adjoint-Based Multistart Approach and Global Gaussian Process Regression
Open the PDF for Robust Optimization of a Compressor Blade Through Combination of an Adjoint-Based Multistart Approach and Global Gaussian Process Regression in another window
Topics: Blades, Compressors, Computational fluid dynamics, Design, Optimization, Rotors, Uncertainty
Proceedings Papers

Probabilistic Analysis of Leading Edge Erosion Behavior of a High-Pressure Compressor in a Turbofan Engine

Andreas Türke, Lukas Schlüter, Matthias Voigt, Robin Schmidt, Andreas Vogel, Ronald Mailach
Proc. ASME. GT2024, Volume 12D: Turbomachinery — Multidisciplinary Design Approaches, Optimization, and Uncertainty Quantification; Radial Turbomachinery Aerodynamics; Unsteady Flows in Turbomachinery, V12DT34A007, June 24–28, 2024
Publisher: American Society of Mechanical Engineers
Paper No: GT2024-122239
https://doi.org/10.1115/GT2024-122239
View Paper titled, Probabilistic Analysis of Leading Edge Erosion Behavior of a High-Pressure Compressor in a Turbofan Engine
Open the PDF for Probabilistic Analysis of Leading Edge Erosion Behavior of a High-Pressure Compressor in a Turbofan Engine in another window
Topics: Compressors, Engines, Erosion, High pressure (Physics), Turbofans, Blades, Geometry, Particulate matter, Dust, Wear
Proceedings Papers

Robust Design Optimization of a Compressor Rotor Using Recursive Cokriging Based Multi-Fidelity Uncertainty Quantification and Multi-Fidelity Optimization

Marcus Wiegand, Andriy Prots, Marcus Meyer, Robin Schmidt, Matthias Voigt, Ronald Mailach
Proc. ASME. GT2024, Volume 12D: Turbomachinery — Multidisciplinary Design Approaches, Optimization, and Uncertainty Quantification; Radial Turbomachinery Aerodynamics; Unsteady Flows in Turbomachinery, V12DT34A006, June 24–28, 2024
Publisher: American Society of Mechanical Engineers
Paper No: GT2024-121977
https://doi.org/10.1115/GT2024-121977
View Paper titled, Robust Design Optimization of a Compressor Rotor Using Recursive Cokriging Based Multi-Fidelity Uncertainty Quantification and Multi-Fidelity Optimization
Open the PDF for Robust Design Optimization of a Compressor Rotor Using Recursive Cokriging Based Multi-Fidelity Uncertainty Quantification and Multi-Fidelity Optimization in another window
Topics: Compressors, Design, Optimization, Rotors, Uncertainty quantification, Robustness, Uncertainty, Blades, Engines, Geometry
Proceedings Papers

Probabilistic CFD Analysis of a High-Pressure Compressor Under Consideration of Manufacturing and In-Service Variability

Lukas Schlüter, Matthias Voigt, Robin Schmidt, Bernd Becker, Ronald Mailach
Proc. ASME. GT2023, Volume 13D: Turbomachinery — Multidisciplinary Design Approaches, Optimization, and Uncertainty Quantification; Radial Turbomachinery Aerodynamics; Unsteady Flows in Turbomachinery, V13DT34A001, June 26–30, 2023
Publisher: American Society of Mechanical Engineers
Paper No: GT2023-100528
https://doi.org/10.1115/GT2023-100528
View Paper titled, Probabilistic CFD Analysis of a High-Pressure Compressor Under Consideration of Manufacturing and In-Service Variability
Open the PDF for Probabilistic CFD Analysis of a High-Pressure Compressor Under Consideration of Manufacturing and In-Service Variability in another window
Topics: Compressors, Computational fluid dynamics, High pressure (Physics), Manufacturing, Shapes, Airfoils, Rotors, Accounting, Blades, Boundary layers
Proceedings Papers

Application of Adjoint-Enhanced First Order Second Moment Method for Robust Design Optimization of a High Pressure Compressor Rotor

Max Dittmann, Robin Schmidt, Marcus Meyer
Proc. ASME. GT2022, Volume 10D: Turbomachinery — Multidisciplinary Design Approaches, Optimization, and Uncertainty Quantification; Turbomachinery General Interest; Unsteady Flows in Turbomachinery, V10DT34A006, June 13–17, 2022
Publisher: American Society of Mechanical Engineers
Paper No: GT2022-80806
https://doi.org/10.1115/GT2022-80806
View Paper titled, Application of Adjoint-Enhanced First Order Second Moment Method for Robust Design Optimization of a High Pressure Compressor Rotor
Open the PDF for Application of Adjoint-Enhanced First Order Second Moment Method for Robust Design Optimization of a High Pressure Compressor Rotor in another window
Topics: Compressors, Design, High pressure (Physics), Optimization, Rotors, Blades, Airfoils, Robustness, Uncertainty, Uncertainty quantification
Proceedings Papers

The Validation of a Parametric Leading Edge Model for Probabilistic CFD Analyses of Post-Service Compressor Airfoils

Lukas Schlüter, Paul Voigt, Matthias Voigt, Ronald Mailach, Robin Schmidt, Mirco Rostamian, Bernd Becker
Proc. ASME. GT2022, Volume 10D: Turbomachinery — Multidisciplinary Design Approaches, Optimization, and Uncertainty Quantification; Turbomachinery General Interest; Unsteady Flows in Turbomachinery, V10DT34A003, June 13–17, 2022
Publisher: American Society of Mechanical Engineers
Paper No: GT2022-78309
https://doi.org/10.1115/GT2022-78309
View Paper titled, The Validation of a Parametric Leading Edge Model for Probabilistic CFD Analyses of Post-Service Compressor Airfoils
Open the PDF for The Validation of a Parametric Leading Edge Model for Probabilistic CFD Analyses of Post-Service Compressor Airfoils in another window
Topics: Airfoils, Compressors, Computational fluid dynamics, Shapes, Rotors, Blades, Electromagnetic scattering, Flow simulation, High pressure (Physics), Jet engines
Journal Articles

Application of Adjoint-Enhanced First Order Second Moment Method for Robust Design Optimization of a High Pressure Compressor Rotor

Max Dittmann, Robin Schmidt, Marcus Meyer
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. February 2023, 145(2): 021010.
Paper No: TURBO-22-1183
https://doi.org/10.1115/1.4055578
Published Online: October 12, 2022
View Article titled, Application of Adjoint-Enhanced First Order Second Moment Method for Robust Design Optimization of a High Pressure Compressor Rotor
Open the PDF for Application of Adjoint-Enhanced First Order Second Moment Method for Robust Design Optimization of a High Pressure Compressor Rotor in another window
Topics: Compressors, Design, Optimization, Rotors, Uncertainty, Blades, High pressure (Physics)
Journal Articles

Comparison of Two Methods for Sensitivity Analysis of Compressor Blades

Robin Schmidt, Matthias Voigt, Konrad Vogeler, Marcus Meyer
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research-Article
J. Turbomach. November 2017, 139(11): 111006.
Paper No: TURBO-17-1065
https://doi.org/10.1115/1.4037127
Published Online: August 16, 2017
View Article titled, Comparison of Two Methods for Sensitivity Analysis of Compressor Blades
Open the PDF for Comparison of Two Methods for Sensitivity Analysis of Compressor Blades in another window
Topics: Blades, Compressors, Flow (Dynamics), Rotors, Sensitivity analysis, Simulation, Geometry, Pressure, Design
Proceedings Papers

Comparison of Two Methods for Sensitivity Analysis of Compressor Blades

Robin Schmidt, Matthias Voigt, Konrad Vogeler, Marcus Meyer
Proc. ASME. GT2016, Volume 7B: Structures and Dynamics, V07BT29A003, June 13–17, 2016
Publisher: American Society of Mechanical Engineers
Paper No: GT2016-57378
https://doi.org/10.1115/GT2016-57378
View Paper titled, Comparison of Two Methods for Sensitivity Analysis of Compressor Blades
Open the PDF for Comparison of Two Methods for Sensitivity Analysis of Compressor Blades in another window
Topics: Blades, Compressors, Sensitivity analysis, Computational fluid dynamics, Simulation, Geometry, Rotors, Shapes, Flow (Dynamics), High pressure (Physics)
Journal Articles

Influence of Chord Length and Inlet Boundary Layer on the Secondary Losses of Turbine Blades

Helmut Sauer, Robin Schmidt, Konrad Vogeler
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. January 2012, 134(1): 011015.
https://doi.org/10.1115/1.4003244
Published Online: May 27, 2011
View Article titled, Influence of Chord Length and Inlet Boundary Layer on the Secondary Losses of Turbine Blades
Open the PDF for Influence of Chord Length and Inlet Boundary Layer on the Secondary Losses of Turbine Blades in another window
Topics: Boundary layers, Cascades (Fluid dynamics), Chords (Trusses), Flow (Dynamics), Displacement, Blades
Proceedings Papers

Influence of Chord Length and Inlet Boundary Layer on the Secondary Losses of Turbine Blades

Helmut Sauer, Robin Schmidt, Konrad Vogeler
Proc. ASME. GT2010, Volume 7: Turbomachinery, Parts A, B, and C, 1089-1100, June 14–18, 2010
Publisher: American Society of Mechanical Engineers
Paper No: GT2010-22065
https://doi.org/10.1115/GT2010-22065
View Paper titled, Influence of Chord Length and Inlet Boundary Layer on the Secondary Losses of Turbine Blades
Open the PDF for Influence of Chord Length and Inlet Boundary Layer on the Secondary Losses of Turbine Blades in another window
Topics: Boundary layers, Chords (Trusses), Turbine blades, Cascades (Fluid dynamics), Flow (Dynamics), Computational methods, Deflection, Displacement, Friction, Integral equations