- 2023
- 2022
- 2021
- 2020
- 2019
- 2018
- 2017
- 2016
- 2015
- 2014
- 2013
- 2012
- 2010
- 2009
- 2008
- 2007
- 2006
- 2005
- 2004
- 2003
- 2002
- 2001
- 2000
- 1999
- 1998
- 1997
- 1996
- 1995
2023
- Numerical Investigation of the Influence of the Degree of Reaction in an Axial Compressor Stage With Tandem Vanes. TUM Lehrstuhl für Turbomaschinen und Flugantriebe, 2023, mehr…
- Numerical Investigation of the Influence of the Degree of Reaction in an Axial Compressor Stage With Tandem Vanes. TUM Lehrstuhl für Turbomaschinen und Flugantriebe, 2023, mehr…
- High-Fidelity Simulation and Flow Analysis of a Low-Pressure Turbine Cascade in a Spanwise-Diverging Gas Path - Part I: Calibration of Inlet Boundary Conditions. 23rd Australasian Fluid Mechanics Conference - 23AFMC, 2023 mehr…
- Experimental investigation of performance and soot emissions of oxygenated fuel blends in a small aero engine. TUM Lehrstuhl für Turbomaschinen und Flugantriebe, 2023, mehr…
- Detailed Gaseous and Particulate Emissions of an Allison 250-C20B Turboshaft Engine. Journal of Engineering for Gas Turbines and Power., 2023 mehr…
- Challenges in the Application of Hot-Wire Anemometry for the Investigation of Transient Temperature Fluctuations in a High-Speed Research Compressor. ASME Turbo Expo, American Society of Mechanical Engineers, 2023 mehr…
- Design of a small pressure chamber to evaluate probe calibrations at varying Reynolds numbers. Journal of Physics: Conference Series 2511 (1), 2023, 012023 mehr…
2022
- Numerical Investigation of Near-Tip Modifications for a Highly Loaded Low-Speed Rotor Under the Influence of Double Leakage. Journal of Turbomachinery, 2022 mehr…
- Platform Leakage and Blade Tilting in Axial Compressor CFD-Simulations. 25th Conference of the International Society for Air Breathing Engines, 2022 mehr…
- Numerical Analysis of Blade Platform Leakage in Axial Compressors. ASME Turbo Expo 2022 Turbomachinery Technical Conference and Exposition, 2022 mehr…
- Analysis of Cavity Leakage Effects on Coupled Non-Axisymmetric Endwall-Arifoil Optimization in a Low-Speed Compressor Tandem Stator. ASME, 2022 mehr…
- Influence of additive surface area degradation on fine particle formation during biomass pulverised-fuel combustion. Elsevier, 2022 mehr…
- Robust Optimization Used in the Redesign of a Low-Speed Compressor Tandem Stator. ISABE 2022, 25th ISABE Conference, 2022 mehr…
- Numerical Calibration and Investigation of the Influence of Reynolds Number on Measurements With Five-Hole Probes in Compressible Flows. Journal of Turbomachinery 144 (9), 2022 mehr…
- Design of a Small Pressure Chamber to Evaluate Probe Calibrations at Varying Reynolds Numbers. XXVI Biennial Symposium on Measuring Techniques in Turbomachinery, 2022 mehr…
2021
- Numerical Investigation of the Aerodynamic Performance of Hybrid Aerofoils in a 1.5-Stage Low-Speed Compressor. Volume 2A: Turbomachinery — Axial Flow Fan and Compressor Aerodynamics, American Society of Mechanical Engineers, 2021 mehr…
- Numerical Investigation of the Aerodynamic Performance of Hybrid Aerofoils in a 1.5-Stage Low-Speed Compressor. ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition, 2021 mehr…
- Blade design and tip clearance flow analysis for a compact high-pressure compressor rear stage. 14th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, European Turbomachinery Society, 2021 mehr…
- Numerical Calibration and Investigation of the Influence of Reynolds Number on Measurements With Five-Hole Probes in Compressible Flows. ASME Turbo Expo, 2021 mehr…
2020
- Effect of Heating on the Stability of the Three-Dimensional Boundary Layer Flow over a Rotating Disk. . Biennial Symposium on Measuring Techniques in Turbomachinery Transonic and Supersonic Flow in Cascades and Turbomachines, 2020 mehr…
- Numerical Investigation of Compressor Tandem Aerofoils Featuring Near-Endwall Modification. 18th Symposium on Transport Phenomena and Dynamics of Rotating Machinery ISROMAC, 2020 mehr…
- Helicpoter Engine Performance Simulations Accounting for Intake Distortion. Deutscher Luft- und Raumfahrtkongress DLRK, 2020 mehr…
- Design of a rear-stage subsonic axial compressor with casing treatments. CEAS Aeronautical Journal (ISSN 1869-5582), 2020 mehr…
- Experimental Investigation of the Starting Provedure of a Helicopter Gas Turbine Featuring an Impingment Quick-start System. ASME Turbo Expo 2020, 2020 mehr…
- Reduced-Order Modelling of Rotating Stall. ASME International Gas Turbine & Aero Engine Technical Congress, 2020 mehr…
- Potential of Surrogate Modeling in Compressor Casing Design Focusing Rapid Tip Clearance Assessments. 65th ASME International Gas Turbine & Aero Engine Technical Congress, 2020 mehr…
- Multi-Objective Optimization and System Evaluation of Recuperated Helicopter Turboshaft Engines. Journal of Energy, 2020 mehr…
- Effect of Heating on the Stability of the Three-Dimensional Boundary Layer Flow over a Rotating Disk. Proceedings of the XXV Biennial Symposium on Measuring Techniques in Turbomachinery, 2020, 10 mehr…
2019
- Interacting Flow Effects in the Stages of a Low-Speed Multistage Axial Compressor Using Shrouded and Cantilevered Stators. 55th AIAA/SAE/ASEE Joint Propulsion Conference, 2019 mehr…
- Preliminary Design of a Three-Stage Low-Speed Research Compressor Using Tandem Vanes. 55th AIAA/SAE/ASEE Joint Propulsion Conference, 2019 mehr…
- Validation of Higher-Order Interactional Aerodynamics Simulations on Full Helicopter Configurations. Journal of the American Helicopter Society Volume 64, Number 4, 2019, 1-13 mehr…
- New Methods for Secondary Flow Phenomena Visualization and Analysis. ASME Turbo Expo, 2019 mehr…
- Design Aspects and Characterization of a Resonance Igniter or Oxygen/Methane in Orbit Propulsion Systems. 8th European Conference for Aeronautics and Space Sciences, 2019 mehr…
- Development and Commissioning of a High-Speed Research Compressor Facility. 55th AIAA/SAE/ASEE Joint Propulsion Conference, 2019 mehr…
- Reducing compressor shroud leakage flow bai raising the stator hub line: low speed tests. ASME Turbo Expo, 2019 mehr…
- Structural Analysis of an Auxetic Casing Structure Incorporating Tip Blowing Casing Treatment Modification. ASME Turbo Expo, 2019 mehr…
- Quantification of the Effect of Circumferential Repeated 3D Features on Radial Displacement of a Compressor Casing Focusing Model Simplification: Part I. 8th International Conference on Mechanics and Industrial Engineering, 2019Paper No. ICMIE 122 mehr…
- The potential of helicopter turboshaft engines incorporating highly effective recuperators under various flight conditions. Aerospace Science and Technology 88, 2019, 84-94 mehr…
- High temperature heat exchangers for recuperated rotorcraft powerplants. Applied Thermal Engineering 154 (25), 2019, 548-561 mehr…
- Optimization design analysis of primary surface recuperator for rotorcraft powerplant applications. ASME Turbo Expo, 2019 mehr…
- Pressure-sensitive paint measurements in narrow clearances - a feasibility study. ASME Turbo Expo, 2019 mehr…
- Stagnation Flow and Heat Transfer From a Finite Disk Situated Perpendicular to a Uniform Stream. Journal of Fluids Engineering 142 (3), 2019, 15 mehr…
2018
- Experimental Investigation of a Radial Turboshaft Engine intake. 54nd AIAA/SAE/ASEE Joint Propulsion Conference, 2018 mehr…
- Experimentelle Untersuchung des Wärmeübergangs an Rotierenden Scheiben. Dissertation, 2018 mehr…
- Experimental study of the influence of the Prandtl number on the convective heat transfer from a square cylinder. International Journal of Heat and Mass Transfer 120, 2018, 471--480 mehr…
- Quick Start - Von 0 auf 30.000 Umdrehungen in 2,6 Sekunden. dSPACE Magazin 1, 2018, 31-35 mehr…
- Control Systems Enables Helicopter Engine Quick Start. Aerospace Testing International, 2018 mehr…
- Higher-Order Simulations of Interactional Aerodynamics on Full Helicopter Configurations Using a Hamiltonian Strand Approach. 44th European Rotorcraft Forum, 2018 mehr…
- Experimental Investigation and Numerical Validation of the Bearing Face Flow of an Adaptive Seal. ASME Turbo Expo, 2018 mehr…
2017
- Prandtl Number Effect on the Laminar Convective Heat Transfer From a Rotating Disk. Journal of Heat Transfer 139 (10), 2017, 10 mehr…
- Using Annulus Contouring to Compensate Compressor Mis-Matching Effects in the Presence of Casing Treatments. 23rd International Symposium on Air Breathing Engines, 2017 mehr…
- Multiobjective topology optimization with the sko-method. Structural and Multidisciplinary Optimization 57, 2017, 325-340 mehr…
- Experimental Investigation of an Engine Quick-Start System with Compact Air Supply for Rotorcraft Application. 17th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, 2017 mehr…
- Operational Aspects of an Engine Quick-Start System with Compact Air Supply for Rotorcraft Application. Deutscher Luft- und Raumfahrtkongress, 2017 mehr…
- Improved flammability for hydrogen fuelled scramjets with preinjection catalytic radical farming. 23rd International Symposium on Air Breathing Engines, 2017 mehr…
- Analysis of an Auxetic Casing Structure for Tip Clearance Control under Various Temperature and Pressure Conditions. 23rd International Symposium on Air Breathing Engines, 2017 mehr…
- Design of a static test rig for advanced seals and air bearing testing. 17th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, 2017 mehr…
2016
- Entwicklung eines evolutionären Algorithmus zur Mehrziel-Topologieoptimierung. 3rd German-language NAFEMS Regional Conference, 2016 mehr…
- Fatigue Analysis of a Cylindrical Turbine Disk with Integrated Heat Pipes. 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016 mehr…
- Challenges in designing very small jet engines - fuel distribution and atomization. 16th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, 2016 mehr…
- Effect of Prandtl Number on the Heat Transfer from a Rotating Disk: An Experimental Study. ASME Summer Heat Transfer Conference, 2016 mehr…
- Experimental Investigation of the Laminar Boundary Layer Flow on a Rotating Wavy Disk. ASME Fluids Engineering Division Summer Meeting, 2016 mehr…
- Effect of Prandtl Number on Convective Heat Transfer in the Separated and Reattached Flow Region on a Blunt Flat Plate. ASME Fuids Engineering Division Summer Meeting, 2016 mehr…
- Difference in the Working Principle of Axial Slot and Tip Blowing Casing Treatments. ASME Turbo Expo, 2016GT2016-56966 mehr…
- Investigation On Direct And Hybrid Sound Prediction. ASME Turbo Expo (GT2016-57612), 2016 mehr…
- Evaluation of Future Helicopter Powertrain Concepts Regarding Flight Mission and Operational Aspects. 72nd American Helicopter Society International Annual Forum, 2016 mehr…
- Design of an Airworthy Turboshaft Engine Quick-Start System with Compact Pressurized Air Supply for Rotorcraft Application. 42nd European Rotorcraft Forum, 2016 mehr…
- Design Parameter Identification of the Air Supply for a Turboshaft Engine Quick-Start System. 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016AIAA-2016-5062 mehr…
- Introduction of Circumferentially Nonuniform Variable Guide Vanes in the Inlet Plenum of a Centrifugal Compressor for Minimum Losses and Flow Distortion. Journal of Turbomachinery 138 (9), 2016, 10 mehr…
- Convective Heat Transfer From Rotating Disks Subjected To Streams Of Air. SpringerBriefs in Applied Sciences and Technology Thermal Engineering and Applied Science. Springer International Publishing, 2016 mehr…
2015
- Transient Simulation of a Gas Turbine Disk Incorporating Heat Pipes under Structural Aspects. ASME Turbo Expo, 2015 mehr…
- Rotating Heat Pipes with a Focus on Stress Concentrations. 22nd ISABE Conference, 2015 mehr…
- Influencing Parameters of Tip Blowing Interacting with Rotor Tip Flow. ASME Turbo Expo, 2015 mehr…
- Turbulent Heat Transfer on a Blunt Flat Plate with Passive Jet Injection. 8th International Symposium on Turbulence, Heat and Mass Transfer, Begell House Inc., 2015 mehr…
- Aerodynamic Investigation of a Passive Secondary Jet Exciting a Separation Bubble for a Blunt Flat Plate. ASME/JSME/KSME 2015 Joint Fluids Engineering Conference, 2015 mehr…
- Influence of a Tip Blowing Casing Treatment on the Stator Flow Field. 51st AIAA/SAE/ASEE Joint Propulsion Conference, 2015 mehr…
- Investigation of Engine Operating Behavior after Compressor Casing Modification due to Installation of a Quick-Start System. 22nd ISABE Conference, 2015 mehr…
- Design of an Engine Quickstart System for Rotorcraft Application. 11th European Turbomachinery Conference, 2015 mehr…
- Untersuchungen zu Düsenströmungen kleiner Fluggasturbinen. Deutscher Luft- und Raumfahrtkongress, 2015 mehr…
- Introduction of circumferentially non-uniform variable Guide Vanes in the Inlet Plenum of a centrifugal Compressor for minimum Losses and Flow Distortion. ASME Turbo Expo, 2015 mehr…
2014
- Effect of Blade Tip Modifications for Unducted Propulsors on Tip Vortex-Rotor Interaction Noise. ASME Turbo Expo, 2014 mehr…
- Tailoring Rotor-Rotor Interactions Using Blade Row Spacing for Effects of Destructive Acoustic Interference. 15th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, 2014 mehr…
- Structural Analysis of a Gas Turbine Disk Containing Heat Pipes Using Finite Element Analysis. ASME Turbo Expo, 2014 mehr…
- Parametric Study of the Bleed Position in a Tip Blowing Casing Treatment. ASME Turbo Expo, 2014 mehr…
- Tip Gap Variation on a Transonic Rotor in the Presence of Tip Blowing. ASME Turbo Expo, 2014 mehr…
- Flow Over a Blunt Disk With Incidence: Location of Stagnation Point and Flow Separation. 4th Joint US-European Fluids Engineering Division Summer Meeting, 2014 mehr…
- Convective Heat Transfer From a Free Rotating Disk Subjected to a Forced Crossflow. ASME Turbo Expo, 2014 mehr…
- Internal Symmetries, Fundamental Invariants, and Convective Heat Transfer from a Rotating Disk. 15th International Heat Transfer Conference, 2014 mehr…
- Investigation of Parameters Affecting the Thermodynamic Cycle of Very Small Jet Engines. 15th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, 2014 mehr…
- Evaluation of Helicopter Flight Missions with Intended Single Engine Operation. 40th European Rotorcraft Forum, 2014 mehr…
- Application of Flow Control on a radial Compressor for Operating Range Extension. 15th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, 2014 mehr…
- Numerical Investigations of Hub Treatments for Cantilever Stators. 15th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, 2014 mehr…
- Topology Optimization in Structural Design of a LP Turbine Guide Vane: Potential of Additive Manufacturing for Weight Reduction. ASME Turbo Expo, 2014 mehr…
- Thermo-elastic optimization for additively manufactured turbo machinery components. 7th Annual European Altair Technology Conference, 2014 mehr…
- Performance and Functionality Based Design Methods for Improved and Novel Aircraft Engine Components for Additive Manufacturing. 25th Annual International Solid Freeform Fabrication Symposium, 2014 mehr…
- New Possibilities of Additive Manufacturing in Aero Engine Component Design - Topology Optimized Turbine Stator. Fraunhofer Direct Digital Manufacturing Conference, 2014 mehr…
- Effects on Helicopter Dynamics in Case of Engine Failure During Intended Single Engine Operation. 40th European Rotorcraft Forum, 2014 mehr…
2013
- An evaluation of the potential of additive manufacturing technologies in future aero engine design. ASME Turbo Expo, 2013 mehr…
- Aerodynamic Origin of Rotor-Rotor Interaction Noise from Unducted Propulsors. ASME Turbo Expo, 2013 mehr…
- The effect of the incidence angle on the flow over a rotating disk subjected to forced air streams. ASME Fluids Engineering Division Summer Meeting, 2013 mehr…
- Impact of injection distribution on cryogenic rocket engine stability. Progress in Propulsion Physics 4, 2013, 149-166 mehr…
- Modeling of BO 105 Flight Dynamics for Research on Fuel Saving due to Single-Engine Operation. 39th European Rotorcraft Forum, 2013 mehr…
- Evolution of Generic Vanelets Applied to a High Pressure Compressor. ASME Turbo Expo, 2013 mehr…
- Aerodynamic Design of Abradable Liners with Integrated Endwall Treatments for Axial Compressor Rotors. ASME Turbo Expo, 2013 mehr…
- An Evaluation of the Potential of Additive Manufacturing Technologies in Future Aero Engine Design. ASME Turbo Expo, 2013 mehr…
- Numerical Investigation of an Additively Manufactured Compressor Casing: The Effect of Auxetic Structures on the Tip Clearances. ASME Turbo Expo, 2013 mehr…
- An advanced axial-slot casing treatment on a transonic compressor – A close look with computational fluid dynamics and experimental validation. ASME Turbo Expo, 2013 mehr…
- Axial-Slot Casing Treatments Improve the Efficiency of Axial Flow Compressors: Aerodynamic Effects of a Rotor Redesign. ASME Turbo Expo, 2013 mehr…
- Untersuchung der Exzentrizität von Gehäuseringen infolge statistisch verteilter Fertigungsabweichungen. Deutscher Luft- und Raumfahrtkongress, 2013 mehr…
- Statistical Impact of Manufacturing Tolerances on Axial Gaps Between Vane Segments and the Rotor of Axial Flow Turbo-Compressors. ASME Turbo Expo, 2013 mehr…
2012
- Instationäre numerische Untersuchung der aerodynamischen Rotor-Stator-Interaktion in einem Radialverdichter. Dissertation, 2012 mehr…
- Unsteady Aerodynamics of a Centrifugal Compressor Stage - Validation of Two Different CFD Solvers. ASME Turbo Expo, 2012GT2012-69636 mehr…
- Influence of Discretisation on the Prediction of Propeller Noise Generation: Theory and Application. 14th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, 2012ISROMAC-2012-1135 mehr…
- Investigation of combustor concepts for micro gas turbine jet engines. 23rd International Symposium on Transport Phenomena, 2012 mehr…
- Simulation of Liquid and Transcritical Cooling Films in Rocket Combustion Chambers. Space Propulsion, 2012 mehr…
- Engine Quick Start in Case of Emergency - A Requirement for Saving Fuel by Means of Engine Shutdown. 38th European Rotorcraft Forum, 2012 mehr…
- Near-Field Noise Reduction of a Ducted Helicopter Tail Rotor due to a Modified Stator Vane Geometry. ASME Turbo Expo, 2012GT2012-69118 mehr…
- Aeroacoustic Near-Field Study of a Ducted Helicopter Tail Rotor with Different Vane Count by Use of Phase-Lagged Boundaries. 14th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, 2012ISROMAC-2012-1152 mehr…
- Modeling of BO 105 Flight Dynamics for Research on Fuel Saving due to Single-Engine Operation. 38th European Rotorcraft Forum, 2012 mehr…
- Assessment of Analytical Models for Film Cooling in a Hydrocarbon/ GOX Rocket Combustion Chamber. 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2012 mehr…
- Experimental Investigation on Film Cooling in a Hydrocarbon/ GOX Rocket Combustion Chamber. 50th AIAA Aerospace Sciences Meeting and Exhibit, 2012AIAA-2012-0526 mehr…
- Simulation des Schwungrad-Reibschweißprozesses mit ABAQUS. Forschung im Ingenieurwesen 76 (3-4), 2012, 67-76 mehr…
- Generativ gefertigte Teile im Flugzeugbau - Neue Ansätze in der Triebwerkskonstruktion. DIGITAL ENGINEERING (4), 2012, 24-25 mehr…
- New possibilities for blade mistuning through the use of additive manufacturing technologies. 13th International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines, 2012 mehr…
- New Possibilities of Aero Engine Design Using Additive Manufacturing Technologies. Fraunhofer Direct Digital Manufacturing Conference, 2012 mehr…
- Effect of Ambient Pressure Fluctuations on Dual-Bell Transition Behavior. 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2012 mehr…
- Using Intra Cooling Channel Measurements for Film Cooling Investigations in a GOX/ Kerosene Rocket Combustion Chamber. 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2012 mehr…
- Using Intra Cooling Channel Measurements for Film Cooling Investigations in a GOX/ Kerosene Rocket Combustion Chamber. Space Propulsion, 2012 mehr…
- Instationäre Strömung im Schaufelrandbereich und in Randkavitäten. 13. Statusseminar der AG Turbo, Wissenschaftliche Koordinierungsstelle AG Turbo - Deutsches Zentrum für Luft-und Raumfahrt e.V. (DLR), 2012 mehr…
- Trading Excessive Stall Margin for Efficiency: An Alternative Approach to Axial-Slot Casing Treatments for Transonic Compressors. 13th International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines, 2012 mehr…
- Teaching Turbo Compressor Design - from Mean Line to 3D CFD. 29th CADFEM ANSYS SIMULATION CONFERENCE, 2012 mehr…
- Investigation of the API-Injection Concept in a LOX/LH2 Combustion Chamber at GG/PB Operation Conditions. 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2012 mehr…
- Analytical Study of Stationary Temperature Field in Transpiration Cooled Porous Wall. Journal of Aerospace Engineering, 2012 mehr…
- Statistische Toleranzeffekte am statorseitigen Axialspaltufer von Turboverdichtern. Deutscher Luft- und Raumfahrtkongress, 2012 mehr…
2010
- Demonstration of an aerodynamic design process for turbomachines using open source software tools. ASME Turbo Expo, 2010GT2010-22194 mehr…
- Implementation of a Domain Scaling Approach for Turbomachinery Computations in OpenFOAM. 5th OpenFOAM Workshop, 2010 mehr…
- Parameter zur Auslegung effizienter Gehäusestrukturierungen. Dissertation, 2010 mehr…
- Numerical Investigation of Unsteady Flow Phenomena in an HP Axial Flow Compressor Incorporating Stator Shroud Cavities. 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2010 mehr…
- Validation of CFD-Simulations for a Supersonic Combustion Chamber using ANSYS CFX. 28th CADFEM ANSYS SIMULATION CONFERENCE, 2010 mehr…
- High Performance Computing in Science and Engineering - Garching Munich 2009 – Comparing Frequency-Based Flow Solution to Traditional Unsteady Fluid Dynamics Analysis in Turbomachinery. In: Springer Science & Business Media, 2010, 161-174 mehr…
- A new fuel/air premixing system for gas turbines and its influences on the performance and emission characteristics. The 21st International Symposium on Transport Phenomena, 2010 mehr…
- Numerical investigation into the unsteady aerodynamics of a ducted helicopter tail rotor under side-wind conditions. ASME Turbo Expo, 2010 mehr…
- Further Experimental and Analytical Results of Film Cooling Investigations with a GOX Kerosene Combustion Chamber. Jahresbericht des SFB Transregio 40 "Technologische Grundlagen für den Entwurf thermisch und mechanisch hochbelasteter Komponenten zukünftiger Raumtransportsysteme", 2010, mehr…
- Entwicklung und Untersuchung eines neuartigen Brennstoffaufbereitungssystems für kleine Gasturbinen. Dissertation, 2010 mehr…
2009
- Numerical Optimization of Compressor Casing Treatments for Influencing the Tip Gap Vortex. In: High Performance Computing in Science and Engineering, Garching/Munich 2007. Springer, 2009, 215--225 mehr…
- Experimental and numerical analysis of axial skewed slot casing treatments for a transonic compressor stage. ASME Turbo Expo, 2009 mehr…
- Experimental investigation on staged injection in a dual-mode combustor. In: Shock Waves. Springer, 2009, 1123--1128 mehr…
- Auslegung und Betriebsverhalten von SCRamjet-Antriebssystemen für Raumtransporter-Hyperschallflugzeuge. Dissertation, 2009 mehr…
- Numerischer Entwurf von effizienten Casing Treatments für einen 4,5-stufigen Hochdruckverdichter. Dissertation, 2009 mehr…
- Validation of the non-linear harmonic approach for quasi-unsteady simulations in turbomachinery. ASME Turbo Expo, 2009 mehr…
- Comparing a 40 Mio gridpoints full-annulus computation with a 7 Mio gridpoints nonlinear harmonic computation. 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition, 2009 mehr…
- Improved prediction of heat transfer in a rocket combustor for GOX/kerosene. 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition, 2009AIAA-2009-1214 mehr…
- Investigation on Film Cooling in a Kerosene/GOX Combustion Chamber. 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2009 mehr…
- Cooling of Ceramic Combustion Chambers. 19th International Society for Air Breathing Engines Conference, 2009ISABE-2009-1159 mehr…
- Experimental Study on Staged Injection in a Supersonic Combustor. 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, 2009AIAA-2009-7343 mehr…
- CMC Materials for Combustion Chamber Applications. EUCASS Advances in Aerospace Sciences - Propulsion Physics, 2009 mehr…
- Scramjet research activities at the Institute of Flight Propulsion of the Technische Universität München. 6th European Symposium on Aerothermodynamics for Space Vehicles, 2009 mehr…
- First Experimental and Analytical Results of Film Cooling Investigations with a GOX/Kerosene Combustion Chamber. Jahresbericht des SFB Transregio 40 "Technologische Grundlagen für den Entwurf thermisch und mechanisch hochbelasteter Komponenten zukünftiger Raumtransportsysteme", 2009, mehr…
- Experimental investigation of cooling techniques and materials for highspeed flight propulsion systems. 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, 2009AIAA-2009-7374 mehr…
- Methoden statistischer Toleranzanalyse bei der Entwicklung von Turbomaschinen. Dissertation, 2009 mehr…
2008
- Implementation of rotor-stator interfaces in OpenFOAM. 3rd OpenFOAM Workshop, 2008 mehr…
- Time resolved simulation and experimental validation of the flow in axial slot casing treatments for transonic axial compressors. ASME Turbo Expo, 2008 mehr…
- NUMERISCHE AUSLEGUNG VON GEHäUSESTRUKTURIERUNGEN FüR EINE TRANSSONISCHE AXIALVERDICHTERSTUFE. Deutscher Luft- und Raumfahrtkongress, 2008 mehr…
- 1D und 3D-Simulationen zur Leistungsvorhersage von Scramjet-Antriebssystemen. Deutscher Luft- und Raumfahrtkongress, 2008 mehr…
- Simulation of casing treatments of a transonic compressor stage. International Journal of Rotating Machinery 2008, 2008 mehr…
- Simulation of casing treatments of a transonic compressor stage. International Journal of Rotating Machinery 2008, 2008, 10 mehr…
- Numerical design and optimization of casing treatments for transonic axial compressors. 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2008AIAA-2008-5063 mehr…
- Development of circumferential grooves for axial compressors based on flow mechanisms. 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2008 mehr…
- Kupfer--Ein Werkstoff fur Raketenbrennkammern. Metall - Internationale Fachzeitschrift für Metallurgie 62 (10), 2008, 646 mehr…
- Design and Commissioning of a Combustion Chamber for Cooling and Material Investigations. 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2008 mehr…
- Prediction and analysis of heat transfer in small rocket chambers. 46th AIAA Aerospace Sciences Meeting and Exhibit, 2008 mehr…
- Gestufte Verbrennung in einer überschallbrennkammer. Deutscher Luft- und Raumfahrtkongress, 2008DLRK2008-81297 mehr…
- Staged injection in a dual-mode combustor for an air-breathing engine. 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2008 mehr…
- Injektoren für Hauptstromtriebwerke mit oxidatorreicher Vorverbrennung. Dissertation, 2008 mehr…
- UNTERSUCHUNG EINES NEUARTIGEN BRENNSTOFF-AUFBEREITUNGSSYSTEMS FüR GASTURBINEN. Deutscher Luft- und Raumfahrtkongress, 2008 mehr…
- Spoke Centering Eccentricity - Statistical Tolerance Analysis. 12th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, 2008ISROMAC12-2008-20025 mehr…
- Investigation in the Eccentricity of Spoke Centered Turbomachinery Components. ASME Turbo Expo, 2008 mehr…
2007
- Re-entry body drag: shock tunnel experiments and computational fluid dynamics calculations compared. Shock Waves 16 (6), 2007, 431--443 mehr…
- Aero-Thermodynamical design of a Scramjet for Future Space Transportation Systems: The Graduate School 1095/1 Funded by the" Deutsche Forschungsgemeinschaft"(DFG). ISABE, 2007, mehr…
- German Test Facilities for High Speed Air Breathing Propulsion. 2nd European Conference for Aerospace Sciences, 2007 mehr…
- Kraftstoffeinspritzsysteme für Vormischbrenner kleiner Fluggasturbinen. Dissertation, 2007 mehr…
- Experimental Investigations on Staged Injection in a Dual Mode Combustor. 26th International Symposium on Shock Waves, Bd, 2007 mehr…
- Combustion stability characteristics of coax-swirl-injectors for oxygen/kerosene. 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2007AIAA-2007-5563 mehr…
- Experimental Investigations of Coax Swirl Injectors for Hydrocarbons. 58th International Astronautical Congress, 2007IAC-07-C4. 3.06, mehr…
- Optimierung der Spiele und Spalte im Konstruktionsprozess von Flugtriebwerken. Dissertation, 2007 mehr…
2006
- Experimental Investigations on Lean Premixed Prevaporized Combustors for Small Aeroengines. 11th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, 2006Paper No. 61 mehr…
- Designing a Casing Treatment for a Transonic Axial Compressor. von Karman Institute for Fluid Dynamics, 2006 mehr…
- Experimental Research on Key technologies for Future Launcher Propulsion. 57th International Astronautical Congress, 2006IAC-06-C4.1.05 mehr…
- Influence of Coaxial Injector Element Design on Heat Transfer in Oxidizer Rich Staged Combustion Cycle Engines. 57th International Astronautical Congress, 2006IAC-06-C4.3.05 mehr…
- Influence of Injector Element Design on Heat Transfer. 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2006 mehr…
- Das Graduiertenkolleg 1095/1:" Aerothermodynamische Auslegung eines Scramjet-Antriebssystems für Zukünftige Raumtransportsysteme. Deutscher Luft- und Raumfahrtkongress, 2006DGLR-2006-127 mehr…
2005
- Numerical evaluation of important parameters ruling the effectiveness of casing treatments in transonic compressors. 17th Symposium on Airbreathing Engines, paper ISABE-2005-1095, Munich, Germany, 2005 mehr…
- Using a multi-level tailored design process to develop a customer satisfaction survey for university evaluation. , 2005 mehr…
- Hypersonic highly integrated propulsion systems--design and off-design simulation. Chapter 5.3. 2. Basic Research and Technologies for Two-Stage-to-Orbit Vehicles. DFG, Wiley-VCH, 2005 mehr…
- Free Stream Investigations on Methane Combustion in a Supersonic Air Flow. AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference, 2005 mehr…
- Characterisation of Main Chamber Injectors for GOX/Kerosene in a Single Element Rocket Combustor. 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2005 mehr…
- Characterisation of combustion and heat transfer using GOx/kerosene in a single-element rocket combustor. 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2005 mehr…
- Numerically aided design of a high-efficient casing treatment for a transonic compressor. ASME Turbo Expo, 2005 mehr…
- Verdichterstabilisierung mit passiven Gehäusestrukturen: eine numerische Analyse. Scientific research dissertation, Lehrstuhl für Flugantriebe, Technische Universität München, München, Germany, 2005 mehr…
2004
- Betriebsverhalten einer Dualmodus-SCRamjet-Modellbrennkammer mit Wasserstoffverbrennung. Dissertation, 2004 mehr…
- Stall margin enhancing flow mechanisms in a transonic compressor stage with axial casing slots. 10 th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, ISROMAC10-2004-006, Honolulu, 2004 mehr…
2003
- Transition between Ramjet and Scramjet Modes in a Combustor for an Air-Breathing Launcher. AIAC Paper 54, 2003 mehr…
- Experimental study on transition between ramjet and scramjet modes in a dual-mode combustor. In: 12th AIAA International Space Planes and Hypersonic Systems and Technologies. , 2003, 7048 mehr…
- Früherkennung aerodynamischer Verdichterinstabilitäten mittels Wavelet-Transformationsregeln. Dissertation, 2003 mehr…
- A numerical investigation of the flow mechanisms in a HPC front stage with axial slots. ASME Turbo Expo, 2003 mehr…
- A numerical investigation of the flow mechanisms in a HPC front stage with axial slots. ASME Turbo Expo, 2003 mehr…
2002
- Flame stabilization in supersonic combustion. (AIAA/AAAF 11th Int. Space Planes and Hypersonic Systems and Technol. Conference), 2002, 2002 mehr…
- Experimental Investigation on Supersonic Combustion with Strut Injection. AIAA 5242, 2002, 2002 mehr…
- Non-intrusive measurements of a LPP combustor under elevated pressure conditions. ASME Turbo Expo, 2002 mehr…
- Modellbasierte Regelung der Hochleistungstriebwerke von Hyperschallflugzeugen. Dissertation, 2002 mehr…
- Untersuchungen zur Verbrennung von Kerosin in Raketentriebwerken. Deutscher Luft- und Raumfahrtkongress, 2002 mehr…
- A numerical investigation of the influence of casing treatments on the tip leakage flow in a HPC front stage. ASME Turbo Expo, 2002 mehr…
2001
- Auslegung und deterministische Optimierung stark gekühlter Turbinen. Dissertation, 2001 mehr…
- Untersuchungen zu LPP-Flugtriebwerksbrennkammern unter erhöhtem Druck. Dissertation, 2001 mehr…
- Eintrittsstörungen bei Fluggasturbinen unter besonderer Berücksichtigung instationärer Gaszusammensetzungen. Dissertation, 2001 mehr…
- Wechselwirkung zwischen Rotorströmung und Casing Treatment. Deutscher Luft- und Raumfahrtkongress, 2001 mehr…
2000
- Einfluß des Drucks auf die Emissionscharakteristik von LPP-Brennern. Deutscher Luft- und Raumfahrtkongress, 2000 mehr…
- Using sweep and dihedral to control three-dimensional flow in transonic stators of axial compressors. ASME Turbo Expo, 2000 mehr…
- Dynamische Echtzeit-Leistungssyntheserechnung mit Sekundär-und Störeffekten für Hyperschall-Luftstrahlantriebe. Dissertation, 2000 mehr…
- Vorhersage von Instandhaltungskosten bei der Auslegung ziviler Strahltriebwerke. Dissertation, 2000 mehr…
- Monitoring of critical inlet air conditions for helicopter gas turbines. 20th Symposium Aircraft Integrated Monitoring Systems, 2000 mehr…
- Vorhersage von Instandhaltungskosten bei der Auslegung ziviler Strahltriebwerke. Dissertation, 2000 mehr…
- Einsatz deterministischer Optimierungsverfahren bei der Vorauslegung hochbelasteter Turbomaschinen. Dissertation, 2000 mehr…
- CFD-Simulationen von Verdichterstufen mit Casing Treatment. Deutscher Luft- und Raumfahrtkongress, 2000 mehr…
1999
- Auslegung und Konstruktion einer Modellbrennkammer zur Untersuchung der Wasserstoffverbrennung in Überschallströmungen. Deutscher Luft- und Raumfahrtkongress, 1999 mehr…
- Monitoring and control of helicopter engines at abnormal operating conditions. RTO Meeting proceedings, 1999 mehr…
- Deterministic optimisation of multiple-stage high-performance turbine-comparative results obtained from parameter and optimisation studies. Deterministische Optimierung einer mehrstufigen Hochleistungsturbine-Vergleichsergebnisse aus Parameter-und Optimierungsstudien. , 1999 mehr…
- Zur Modellierung von Drallflammen einschließlich der NO x-Formation in Flugtriebwerksbrennkammern. Dissertation, 1999 mehr…
1998
- Betriebsverhalten von Wellenleistungsgasturbinen bei Verdichterinstabilitäten und Methoden zur Restabilisierung. Dissertation, 1998 mehr…
- Propulsion/aircraft integration of hypersonic vehicles enabling active thrust vectoring and realtime simulation of dynamic engine bevaviour. Int. J. Turbo Jet Engines, 1998 mehr…
- Compressor matching and designing for tip clearance. NASA (19980219359), 1998 mehr…
- The multidisciplinary design process. RTO LECTURE SERIES, 1998, 1--1 mehr…
- Teillastverhalten einer Überschall" brennkammer mit Wasserstoffverbrennung in Über- und Hyperschallantrieben. Teilprojekt B12, Sonderforschungsbereich 255, 1998 mehr…
- Laserspektroskopische Untersuchungen im Primärteil einer Flugtriebwerks-Brennkammer. Dissertation, 1998 mehr…
- Leistungsberechnung und Betriebsverhaltensanalyse luftatmender Antriebssysteme für Hyperschallflugzeuge im Normalbetrieb und bei Störungen. Arbeits--und Ergebnisbericht, Sonderforschungsbereich 255, Teilprojekt B1, 1998, 233--296 mehr…
1997
- The BR 710, an environmentally friendly engine. CASI-Annual Conference, 1997 mehr…
- Zur Integration des Antriebes in ein Hyperschallflugzeug unter besonderer Berücksichtigung der Kräftebilanzierung. Dissertation, 1997 mehr…
- Mischung und Verbrennung in schadstoffarmen Brennkammern-Untersuchungen an Brennkammern mit Stufung sowie mit Vorvermischung/Vorverdampfung. Deutscher Luft- und Raumfahrtkongress, 1997 mehr…
- Simulationsmodelle zur Regelung von Antriebssystemen für Hochgeschwindigkeitsflugzeuge. 3. Hyperschall-Workshop SFB, 1997 mehr…
- Simulation des Betriebsverhaltens von Antrieben für Raumtransporter, Hyperschallflugzeuge. Dissertation, 1997 mehr…
- DIAGNOSTICS OF NON-REACTING AND REACTING SUPERSONIC FLOWS IN A SCRAMJET MODEL COMBUSTOR USING NON-INTRUSIVE SPECTROSCOPIC METHODS. International Journal of Energetic Materials and Chemical Propulsion 4 (1-6), 1997 mehr…
- Zur Modellierung des Schadstoff-Emissionsverhaltens von Fluggasturbinen. Dissertation, 1997 mehr…
- Neue Technologie für Hubschrauber-Anforderungen an zukünftige Hubschrauberantriebe. , 1997 mehr…
1996
- Modellbildung, Simulation und Entwicklung eines digitalen Reglers für eine Hubschraubergasturbine. Dissertation, 1996 mehr…
- Design and off-design simulation of highly integrated hypersonic propulsion systems. Technische Univ, Advanced Aero-Engine Concepts and Controls p(SEE N 96- 36571 12-07), 1996 mehr…
- Experimental investigation of a SCRAMJET model combustor with injection through a swept ramp using laser-induced fluorescence with tunable excimer lasers. Symposium (International) on Combustion, 1996 mehr…
- Detection of Unburned Hydrocarbons (UHC) in an Atmospheric Pressure Combustor With Premixing and Prevaporization Using a Tuneable Excimer Laser. ASME Turbo Expo, 1996V001T02A012 mehr…
1995
- Simulation and nozzle/afterbody integration of hypersonic propulsion systems. Zeitschrift für Flugwissenschaften und Weltraumforschung 19 (1), 1995, 19--28 mehr…
- Turboshaft Engine Monitoring System including Contingency Operation. 5th European Propulsion Forum, Pisa, 1995 mehr…
- Propulsion/aircraft integration and dynamic performance of hypersonic TSTO-vehicles. 12th International Symposium on Air Breathing Engines, 1995 mehr…
- Zur Echtzeitsimulation von Hyperschallkombinationstriebwerken im Flugsimulator. Deutscher Luft- und Raumfahrtkongress, 1995 mehr…
- One-dimensional model of the chemically reacting flow in a supersonic combustion chamber. Zeitschrift für Flugwissenschaften und Weltraumforschung 19 (1), 1995, 34--40 mehr…
- Thermodynamische Auslegung der Niederdruckturbinen der BR700 Triebwerksfamilie. Deutscher Luft- und Raumfahrtkongress, 1995 mehr…