Conference and Journal Publications
2022
DGLR Kongress 2022, 27.-29.09.2022, Paper DLRK2022_570016
DGLR Kongress 2022, 27.-29.09.2022, Paper DLRK2022_570018
DGLR Kongress 2022, 27.-29.09.2022, Paper DLRK2022_570053
2021
doi:10.1088/1757-899X/1024/1/012068
doi: https://doi.org/10.1115/1.4050118
doi: https://doi.org/10.1115/1.4050116
doi: https://doi.org/10.1115/1.4050330
ETC2021-596, Proceedings of 14th European Conference on Turbomachinery Fluid dynamics & Thermodynamics ETC14,
ETC2021-647, Proceedings of 14th European Conference on Turbomachinery Fluid dynamics & Thermodynamics ETC14,
2020
2019
ETC2019-061, Proceedings of 13th European Conference on Turbomachinery Fluid dynamics & Thermodynamics (ETC13), April 8-12, 2019, Lausanne, Switzerland
J. Turbomach. 141(2), 021004, (Feb. 2019) (7 pages) Paper No: TURBO-18-1034; doi: 10.1115/1.4041132
2018
Int. J. Turbomach. Propuls. Power 2018, 3(1), 5; doi:10.3390/ijtpp3010005
Int. J. Turbomach. Propuls. Power 2018, 3(1), 6; doi:10.3390/ijtpp3010006
Int. J. Turbomach. Propuls. Power 2018, 3(1), 7; doi:10.3390/ijtpp3010007
Int. J. Turbomach. Propuls. Power 2018, 3(1), 8; doi:10.3390/ijtpp3010008
2017
"Experimental Investigation of Pressure Side Flow Separation on the T106C Airfoil at High Suction Side Incidence Flow",
J. Turbomach. 139, issue 5, article 051007, May 2017 (11 pages)
2016
20. DGLR-Fach-Symposium of STAB, STAB2016TR3, Braunschweig, Germany, November 8-9, 2016
J. Eng. Gas Turbines and Power 138, issue 2, article 022605, DOI:10.1115/1.4031305, February 2016 (10 pages)
2015
"CFD Study on the Influence of Geometric and Aerodynamic Parameters on the Ejector Pump Effect"
IGTC2015-018, pp. 1559-1568, Proceedings of the 11th International Gas Turbine Congress 2015, Tokyo (ISBN978-4-89111-008-6), November 15-20, 2015, Tokyo, Japan
"Full Annulus Unsteady CFD Simulations on Effects of Inflow Distortions in a Transonic Axial Compressor Stage"
IGTC2015-090, pp. 683-694, Proceedings of the 11th International Gas Turbine Congress 2015 Tokyo (ISBN978-4-89111-008-6), November 15-20, 2015, Tokyo, Japan
"Comparing the Effect of Unsteady Wakes on Parallel and Divergent Endwalls in a LP Turbine Cascade (T106A-EIZ and T106D-EIZ)"
IGTC2015-137, pp. 979-989, Proceedings of the 11th International Gas Turbine Congress 2015 Tokyo (ISBN978-4-89111-008-6), November 15-20, 2015, Tokyo, Japan
"Aspects of Serpentine Inlets for Integrated Propulsion Systems"
ISABE-2015-20019, Proceedings of the XXII. International Symposium on Air Breathing Engines (ISABE), October 25-30, 2015, Phoenix, AZ, USA
"Influence of Secondary Flow within Integrated Engine Inlets on the Performance and Stability of a Jet Engine"
ISABE-2015-20020, Proceedings of the XXII. International Symposium on Air Breathing Engines (ISABE), October 25-30, 2015, Phoenix, AZ, USA
"CFD Based Comparison of the Aerodynamics within S-Duct Inlet Configurations at Sub- and Full-Scale Engine Test Facilities"
ISABE-2015-20021, Proceedings of the XXII. International Symposium on Air Breathing Engines (ISABE), October 25-30, 2015, Phoenix, AZ, USA
"Numerical Parameter Study on Influences of Geometry Modifications on Performance of Double-S-Shaped Ducts"
ISABE-2015-20022, Proceedings of the XXII. International Symposium on Air Breathing Engines (ISABE), October 25-30, 2015, Phoenix, AZ, USA
"Hochfrequente Mehrkanal-Druckmessungen an einer Triebwerkversuchsanlage"
In: „Virtuelle Instrumente in der Praxis 2015“, VIP-Kongress, Hrsg.: Jamal, R.; Heinze, R., VDE Verlag,
"Aufbau eines MEE-Triebwerk-Prüfstandes mit Zwei-Generatoren-Konzept“
DGLR Kongress 2015, Rostock 22.-24.09.2015, Paper DLRK2015_370051
"Parametric CFD Study on Performance of Double-S-Shaped Ducts with Varying Cross-Sectional Shapes”
ISAIF12-037, 12th International Symposium on Experimental Computational Aerothermodynamics of Internal Flows, 2015
"Aerodynamic Investigations of an Advanced VIGV Design of Adjustabel Geometry for Very High Flow Turning"
GT2015-42166, Proceedings of ASME Turbo Expo 2015: Power for Land, Sea and Air, June 15-19, 2015, Montréal, Canada
"Experimental Investigations on Effects of unsteady Wakes on the Secondary Flows in the linear T106 Turbine Cascade"
GT2015-43170, Proceedings of ASME Turbo Expo 2015: Power for Land, Sea and Air, June 15-19, 2015, Montréal, Canada
"Effects of Flow Distortions as they Occur in S-Duct Inlets on the Performance and Stability of a Jet Engine"
GT2015-42062, Proceedings of ASME Turbo Expo 2015: Power for Land, Sea and Air, June 15-19, 2015, Montréal, Canada
"Hot-Film Measurements on a Low Pressure Turbine Linear Cascade With Bypass Transition"
ASME. J. Turbomach., 2015;137(9):091007-091007-11, doi:10.1115/1.4029967
"Investigating Unsteady Secondary Flows in Linear Low Pressure Turbine Cascade: a Combined Experimental and Numerical Study"
ETC2015-134, Proceedings of the 11th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, 23-27 March 2015, Madrid, Spain
"Analysis of the Influence of Periodic Passing Wakes on the Secondary Flow near the Endwall of a Linear LPT Cascade usign DNS and U-RANS"
ETC2015-151, Proceedings of the 11th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, 23-27 March 2015, Madrid, Spain
2014
"Numerical Simulation of Wing and Nacelle Stall"
"Investigation of a Separated Boundary Layer and its Influence Layerand its Influence on Secondary Flow of a Transonic Turbine Profile"
2013
Koschikow, D.; Fröhlich, J.; Ciorciari, R.; Kirik, I.; Niehuis, R.:
"Numerical and experimental Investigation of the turbulent flow through a low-pressure turbine cascade in the endwall region"
Proceedings in Applied Mathematics and mechanics (PAMM)
Wakelam, Ch.; Hoeger, M.; Niehuis, R.:
"A Comparison of Three Low Pressure Turbine Designs"
Turbo-12-1207, Journal of Turbomachinery Nr.135
MAck, M.; Niehuis, R.; Fiala, A.; Guendogdu, Y.:
"Boundary Layer Control on a Low Pressure Turbine Blade by Means of Pulsed Blowing"
Journal of Turbomachinery Nr. 135
Muth, B.; Niehuis, R.:
"Axial Loss Development in Low Pressure Turbine Cascade"
Journal of Turbomachinery Nr. 135
Grates, D.; Jeschke, P.; Niehuis, R.:
"Numerical Investigations of the Unsteady Flow inside a Centrifugal Compressor Stage with Pipe Diffuser"
GT2013-95465, Proceedings of the ASME Turbo Expo 2013
July 03-06, 2013, San Antonio, TX, USA
Mack, M.; Brachmanski, R.; Niehuis, R.:
"The Effect of Pulsed Blowing on the Boundary Layer Control of a Highly Loaded Low Pressure Turbine Blade"
GT2013-94566, ASME Turbo Expo 2013: Turbine Technical Conference and Exposition
ISBN: 978-0-7918-5522-5
June 03-07, 2013, San Antonio, TX, USA
Gomes, R.; Niehuis, R.:
"Film Cooling on Highly Loaded Blades With Main Flow Separation - Part II: Overall Film Cooling Effectiveness"
Journal of Turbomachinery
Gomes, R.; Niehuis, R.: "Film Cooling on Highly Loaded Blades With Main Flow Separation - Part I: Heat Transfer"
Journal of Turbomachinery
Rademakers, R.; Bindl, S.; Brehm, S.; Muth, B.; Niehuis, R.:
"Investigation of Flow Distortion in an integrated Inlet of a Jet Engine"
DLRK2013_301349, Deutscher Lust- und Raumfahrtkongress 2013
10.09.-12.09.2013, Bonn, Germany
Brachmanski, R.; Niehuis, R.; Gündogdu, Y.:
"Investigation of Secondary FLow and its Influence on the Boundary Layer Transition of a Generic Low-Pressure Turbine Profile"
DLRK2013_301272, Deutscher Luft- und Raumfahrkongress 2013
10.09.12.09.2013, Bonn, Germany
Niehuis, R.; Lesser, A.; Probst, A.; Radespiel, R.; Schulze, S.; Kähler, Ch.; SpieringF.; Kroll, N.; Wartzek, F.; Schiffer, H.-P.:
"Simulation of Nacelle Stall and Engine Response"
ISABE-2013-1402, Proceedings of the XXl. International Symposium on Air Breathing Engines
September 09-13, 2013, Busan, Korea
Muth, B.; Bindl, S.; Brehm, B.; Niehuis, R.:
"Adjusting the Ejector Effence inside a Jet Engine Ground Test Facility - CFD Prediction and Validation"
ISABE-2013-1308, Proceedings of the XXl. International Symposium on Air Breathing Engines
September 09-13, 2013, Busan, Korea
Bindl, S.; Muth, B.; Niehuis, R.:
"Adaption of a Ground Test Facility to Operate a Modern Turbo Jet Engine"
ISABE-2013-1307, Proceedings of the XXl. International Symposium on Air Breathing Engines
September 09-13, 2013, Busan, Korea
Barthmers, S.; Händel, D.; Niehuis, R.; Wacker, Ch.; Klausmann, J.:
"2D Investigation of the Flow Through a Symmetric Variable Inlet Guide Part 2: Numerical Analysis"
AIAA-2013-3683, 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
July 15-17, 2013, San Jose, CA, USA
Händel, D.; Barthmes, S.; Niehuis, R.; Rocstroh, U.; Leopold, L.:
"2D Investigation of the Flow Through a Symmetric Variable Inlet Part 1: Experimental Analysis"
AIAA-2013-3683, 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
ISBN: 978-1-62410-222-6
July 15-17, 2013, San Jose, CA, USA
Gomes, R.; Niehuis, R.:
"The COncept of Adiabatic Heat Transfer Coefficient and its Application to Turbomachinery"
GT2013-94715, Proceedings of ASME Turbo Expo 2013: Turbine Technical Conference and Exposition
ISBN: 978-0-7918-5516-4
June 3-7, 2013, San Antonio, TX, USA
Ciorciari, R.; Kirik, I.; Niehuis, R.:
"Effects of Unsteady Wakes on the Secondary Flows in the linear T106 Turbine Cascade"
GT2013-94768, Proceedings of ASME Turbo Expo 2013: Turbine Technical Conference and Exposition
June 3-7, 2013, San Antonio, TX, USA
Stößel, M.; Bindl. S.; Niehuis, R.:
"Rotating Stall Inception inside the low Pressure Compressor of a Twin-Spool Turbofan Engine"
GT2013-94220, Proceedings of ASME Turbo Expo 2013
ISBN: 978-0-7918-5522-5
June 3-7, 2013, San Antonio, TX, US
2012
Niehuis, R.; Lesser, A.:
"Numerical Simulation of Wing and Nacelle Stall"
High Performance Computing in Science and Engineering
Gomes, R.; Niehuis, R.:
"Heat Transfer and Adiabatic Film Cooling Effectiveness onHighly Loaded High Loaded High Pressure Turbine Blades with Flow Separation"
HT2016-58219, ASME 2012 Heat Transfer Summer collocated with the ASME 2012 Fluids Eningeering Division Summer Meeting and the ASME 2012 10th International Conference on Nanochannels, Microchannels and Minichannels
ISBN: 978-0-7918-4477-9
July 08-12, 2012, Puerto Rico, USA
LesserA.; Ciorciari, R.; Barthmes, S.; Niehuis, R.:
"Numerical Investigaton of the Effect of Inflow Distortion on Transonic Axial Compressor Stage
International Symposium Simulation of Wing and Nacelle Stall
21.06-22.06.2012, Braunschweig; Germany
Muth, B.; Niehuis, R.;
"Axial Loss Development in Low Pressure Turbine Cascades"
GT2012-69726, Proceedings of ASME Turbo Expo 2012: Power for Land, Sea and Air
June 11-15, 2012, Copenhagen, Denmark
Gomes, R.; Niehuis, R.:
"Effects of Periodic Unsteady Inflow on Film Cooling and Heat Transfer on Highly Loaded High Pressure Turbine with Flow Separation"
GT,2012-69390, ASME Turbo Expo 2012: Power for Land, Sea and Air
June 11-15, 2012, Copenhagen, Denmark
Mack, M.; Niehuis, R.; Fiala, A.; Guendogu, Y.:
"Boundary Layer Control on a Low Pressure Turbine Blade by Means of Pulsed Blowing"
GT2012-69029, ASME Turbo Expo 2012: Power for Land, Sea and Air
June 11-15, 2012, Copenhagen, Denmark
Wakelalm, Ch.; Hoeger, M.; Niehuis, R.:
"A Comparison of Three Low Pressure Turbine Designs"
GT2012-69028, ASME Turbo Expo 2012: Power for Land, Sea and Air
June 11-15, 2012, Copenhagen, Denmark
Ciorciari, R.; Lesser, A.; Vlaim, F.; Niehuis, R.:
"Numerical Investigation of Tip Clearance Effects in an Axial Transonic Compressor"
Journal of Thermal Science
Mac, M.; Ludewig, T.; Niehuis, R.:
"Passive Boundary Layer Control of a Thin, Low Pressure Turbine Blade by Pressure to Suction Side Pressure Difference Driven Blowing"
February 27-March 02, 2012, Honolulu, HI, USA
Gomes, R.; Neihuis, R.:
"Aerodynamics of a High-Pressure Turbine Blade with Very High-Pressure Turbine Blade with Very High Loading and Vortex Generators"
Journal of Turbomachinery
Muth, B.; Bindl, S.; Brehm, S.; Niehuis, R.:
"A CFD Study of the Ejector Pump Effect within jet Engine Test Facilities"
ISJPPE 2012
September 10-12, 2012, Xi`an, China
Bindl, S.; Muth, B.; Stößel, M.; Brehm, S.; Niehuis, R.:
"Experimental Investigation on the Ejector Pump Effect in Jet Engine Facilities"
ISJPPE 2012
September 10-12, 2012, Xi`an, China
Blaim, F.; Niehuis, R.:
"Unsteady Simulation of the LP Turbine Test Case T1060D-EIZ using a Transport EEquation based Transition Model"
Deutscher Luft- und Raumfahrtkongress 2012
10.09.-12.09.2020, Berlin, Germany
Lesser, A.; Barthmes, S.; Niehuis, R.:
"Numerical Investigation of the Effect of Inflow Distortions on Transonic Axial Compressor Stages with 2D and 3D Calculations"
28th Congress of the International Council of the Aeronautical Science
September 23-28, 2012, Brisbane, Australia
2011
Niehuis, R.:
"Experimental activities to support CFD tool improvements for Aero Engines"
3rd CEAS Air & Space Conference
Venice, Italy
Bindl, S.; Niehuis, R.:
"Realisierung einer autarken Applikation zur Erkennung und Unterdrückung von Verdichterinstabilitäten"
DGLRK2011-241310, 60. Deutscher Luft- und Raumfahrtkongress
Bremen, Germany
Stößel, M.; Muth, B.; Bindl, S.; Niehuis, R.:
"Basic Study of the Ejector Effect, Part 2:Experimental Approach"
AIAA-2011-5530, 47th AIA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Join Propulsion Conference 2011
ISBN: 978-01-60086-949,5
July 31 - August 03, 2011, San Diego, CA, USA
Muth, B.; Stößel, M.; Beth, S.; Bindl, S.; Niehuis, R.:
"Basic Study of the Ejector Effect. Part 1: CFD"
AIAA-2011-5529, 47th AIA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Join Propulsion Conference 2011
July 31 - August 03, 2011, San Diego, CA, USA
Lesser, A.; Niehuis, R.:
"Detailed Numerical Investigation of a Transonic Axial Compressor Stge with Inlet Distortions"
ISAIF10-106, Proceedings of the 10th International Computational Aerothermodynamics of Internal Flow
July 04-07-2011, Brussels, Belgium
Ciorciari, R.; Lesser, A.; Blaim, F.; Niehuis, R.:
"Tip Clearance Investigation for an Axial Transonic Compressor"
ISAIF10-018, Proceedings of the 10th International Computational Aerothermodynamics of Internal Flow
July 04-07-2011, Brussels, Belgium
Gomes, R.; Niehuis, R.:
"Film Cooling on Highly Loaded Blades with Main Flow Separation - Part 2: Overall Film Cooling Evectiveness"
GT2011-45477, ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition Volume 5: Heat Transfert, Parts A and B
ISBN: 978-0-7918-5465-5
June 06-10, 2011, Vancouver, BC. Canada
Gomes, R.; Niehuis, R.:
"Film Cooling on Highly Loaded Blades with Main Flow Separation - Part i: Heat Transfer"
GT2011-45476, ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition Volume 5: Heat Transfert, Parts A and B
ISBN: 978-0-7918-5465-5
June 06-10, 2011, Vancouver, BC. Canada
Montis, M.; Niehuis, R.; Fiala, A.:
"Aerodynamic Measurements on a Low Pressure Turbine Cascade with Different Levels of Distributed Levels on Distributed Roughness"
GT2011-45015, ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition Volume 7: Turbomachinery, Parts A, B and C
ISBN: 978-0-7918-5467-9
June 06-10, 2011, Vancouver, BC. Canada
Lesser, A.; Iseler, J.; Niehuis, R.:
"Numerical Investigation of a Highly Loaded Axial Compressor Stage With Inlet Distortions"
GT2011-46457, ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition Volume 7: Turbomachinery, Parts A, B and C
ISBN: 978-0-7918-5467-9
June 06-10, 2011, Vancouver, BC. Canada
Mack, M.; Niehuis, R.; Fiala, A.:
"Parametric Study of Fluidic Oscillators for Use in Active Boundary Layer Control"
GT2011-45073,
ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition Volume 7: Turbomachinery, Parts A, B and C
ISBN: 978-0-7918-5467-9
June 06-10, 2011, Vancouver, BC. Canada
Ludewig, T.; MAck, M.; Niehuis, R.; Franke, M.:
"Optimization of the Blowing Ratio for a Low Pressure Turbine Cascade with Active Flow Control"
ETC_2011_131, Proceedings 9th European Turbomachinery Conference
March 21-25, 2011, Istanbul, Turkey
Montis, M.; Ciorciari, R.; Niehuis, R.; Salvadori, S.; Carnevale, M.; Mertelli, F.:
"Aerothermal Analysis of Suction Side Film Cooling in a High-Pressure Nozzle Guide Vane Cascade"
ETC_2011_046,
Proceedings 9th European Turbomachinery Conference
March 21-25, 2011, Istanbul, Turkey
Gomes, R.; Niehuis, R.:
"Film Cooling Effectiveness Measurements with Periodic Unsteady Inflow on Highly Loaded Blades with Main Flow Separation"
Journal of Turbomachinery Nr. 133
Lieser, J.; Schulze, S.; Kähler, Ch.; Biela, C.; Lesser, A.; Niehuis, R.:
"Compressor Rig Test with Distorted Inflow Using Distortion Generators"
DGLRK2011-241449
2010
Ludewig, T., Niehuis, R., Franke, M.:
"Comparison of the Capability of Active and Passive Methods of Boundary Layer Control on a Low Pressure Turbine Cascade"
published in Series “Notes on Numerical Fluid Mechanics and Multidisciplinary De-sign”, Vol. 112, Springer Verlag 2010, pp. 191-198, ISBN 978-3-642-14242-0
(peer reviewed paper of 16th STAB/DGLR Symposium Aachen, Germany 2008)
Stößel, M., Niehuis, R.:
"Einrichtung einer Messdatenerfassungsanlage mit Online-Datenservereigenschaften mittels NI PXI und LabVIEW Real-Time"
in „Virtuelle Instrumente in der Praxis 2010“, VIP-Kongress, Hrsg.: Jamal, R., Heinze, R., VDE Verlag,
ISBN 978-3-8007-3235-7, pp. 25-29, 2010
Stößel, M., Rottmann, Th., Niehuis, R.:
"Anpassung von Treibersoftware zur Ansteuerung und TCP/IP-Kommunikation mit Netscannerelementen in LabVIEW"
in „Virtuelle Instrumente in der Praxis 2010“, VIP-Kongress, Hrsg.: Jamal, R., Heinze, R., VDE Verlag,
ISBN 978-3-8007-3235-7, pp. 21-24, 2010
Bindl, S., Niehuis, R.:
"Numerical Investigation of a Transonic Axial Compressor Stage with Inlet Distor-tions"
Workshop "15 Jahre NGV Dresden – Forschung zur Verdichteraerodynamik"
TU Dresden 05.11.2010
Lesser, A., Schulze, S., Niehuis, R., Kähler, Ch., Lieser, J.:
„Design and Numerical Simulation of an Inlet Distortion Generator”
17. DGLR-Fach-Symposium der STAB, Berlin 09./10.11.2010
Stößel, M., Bindl, S., Muth, B., Niehuis, R.,
"Charakterisierung von Leistungsgrenzen für Prüfstände von Turbostrahltriebwerken anhand von Strömungs- und Schwingungskenngrößen"
DLRK2010-1246, Deutscher Luft- und Raumfahrtkongress, August 31-September 2, 2010, Hamburg, Germany
Lesser, A., Iseler, J., Niehuis, R.:
"Numerical Investigation of a Transonic Axial Compressor Stage with Inlet Distortions"
Joint Symposium of DFG FOR 1066 and DLR-Airbus C²A²S²E², Braunschweig, Germany, 2010
Sousek, J., Pfitzner, M., Niehuis, R.:
"Experimental Study of Discharge Coefficients of Radial Orifices in High-Speed Rotating Shafts"
GT2010-22691, Proceedings of ASME Turbo Expo 2010: Power for Land, Sea and Air, June 14-18, 2010, Glasgow, UK
Montis, M.; Niehuis, R.; Fiala, A.:
"Effect of Surface Roughness on Loss Behaviour: Aerodynamic Loading and Boundary Layer Development of a Low-Pressure Gas Turbine Airfoil"
GT2010-23317, Proceedings of ASME Turbo Expo 2010: Power for Land, Sea and Air, June 14-18, 2010, Glasgow, UK
Martinstetter, M.; Niehuis, R.; Franke, M.:
"Passive Boundary Layer Control on a Highly Loaded Low Pressure Turbine Cascade"
GT2010-22739, Proceedings of ASME Turbo Expo 2010: Power for Land, Sea and Air, June 14-18, 2010, Glasgow, UK
Schwarze, M.; Niehuis, R.:
"Numerical Simulation of a Highly Loaded LPT Cascade With Strong Suction Side Separation Under Periodically Unsteady Inflow Conditions"
GT2010-22363, Proceedings of ASME Turbo Expo 2010: Power for Land, Sea and Air, June 14-18, 2010, Glasgow, UK
Gomes, R. A.; Niehuis, R.:
"Aerothermodynamics of a High-Pressure Turbine Blade With Very High Loading and Vortex Generators"
GT2010-23543, Proceedings of ASME Turbo Expo 2010: Power for Land, Sea and Air, June 14-18, 2010, Glasgow, UK
Bindl, S., Muth, B. und Niehuis, R.:
Recirculation of Bleed Air for Active Compressor Stabilization
The 13th ISROMAC Conference, ISROMAC-2010-13, USA, Honolulu, HI, 4-7 April, 2010
Muth, B., Bindl, S. und Niehuis, R.:
CFD Study on an Air Injection System for Active Compressor Stabilisation
The 13th ISROMAC Conference, ISROMAC-2010-13, USA, Honolulu, HI, 4-7 April, 2010
2009
Iseler, J., Lesser, A. Niehuis, R.:
„Numerical Investigation of a Transonic Axial Compressor Stage with Inlet Distortions”,
In: Wagner, S., Steinmetz, M., Bode, A., Müller, M.M.: High Performance Computing in Science and Engineering, Garching/Munich 2009, Springer Verlag, ISBN 978-3-642-13871-3, 2010
Martinstetter, M.:
Reduktion der Verluste hoch belasteter Niederdruckturbinen-Gitter durch Einsatz passiver Turbulatoren
Vortrag beim Seminar für Flugantriebe und Gasturbinen, TU München, Garching, 22. Oktober 2009
Bindl, S., Muth, B., Niehuis, R.:
Instrumentation of a Twin-Spool Turbofan Engine for Compressor Stall Detection EVI2009-004, The 4th EVI-GTI International Gas Turbine Instrumentation Conference, 23.-25. September, 2009, Norrköping, Sweden
Bindl, S., Muth, B., Rottmann, T., Niehuis, R.:
Adaptierung einer Triebwerkversuchsanlage für die Inbetriebnahme eines MEE (More Electric Engine) Demonstratortriebwerks
DLRK2009-121178, Deutscher Luft- und Raumfahrtkongress, 08.-10. September, 2009, Aachen, Deutschland
Muth, B., Bindl, S., Ludwig, S., Niehuis, R.:
CFD-Studien eines Lufteinblasesystems zur Unterdrückung von Verdichterinstabilitäten
DLRK2009-121182, Deutscher Luft- und Raumfahrtkongress, 08.-10. September, 2009, Aachen, Deutschland
Bindl, S., Muth, B., Niehuis, R.:
Active Stall Elimination by Air Injection onto the Tip Region of Compressor Blades
ISABE-2009-1105, Proceedings of the XIX. International Symposium on Air Breathing Engines (ISABE), September 7-11, 2009, Montreal, Canada
Muth, B., Bindl, S., Opterwinkel, N., Niehuis, R.:
Numerical investigation of the aerodynamic conditions inside a sea level engine test facility operating a modern jet engine
ISABE-2009-1214, Proceedings of the XIX. International Symposium on Air Breathing Engines (ISABE), September 7-11, 2009, Montreal, Canada
Schwarze, M.; Martinstetter, M.; Niehuis, R.:
Modeling the Influence of Inflow Turbulence on LPT Performance
AIAA-2009-4930, Proceedings of the AIAA Joint Propulsion Conference & Exhibit, August 3-5, Denver, CO, USA
Bindl, S., Muth, B., Niehuis, R.”:
Experimental Investigations on Macro-Aerodynamics Within a Jet Engine Ground Test Facility”
AIAA-2009-4828, Proceedings of the AIAA Joint Propulsion Conference & Exhibit, August 3-5, Denver, CO, USA
Muth, B., Bindl, S., Lehmann, Ch., Niehuis, R.:
”Numerical Investigation of Inlet Induced Distortions of a Turbofan Engine Within an Indoor Test Facility”
AIAA-2009-4826, Proceedings of the AIAA Joint Propulsion Conference & Exhibit, August 3-5, Denver, CO, USA
Niehuis, R., Iseler, J., Lesser, A.:
„Numerical Investigation of a Highly Loaded Axial Compressor Stage with Inlet Distortions“,
Zeitschriftenartikel in inSiDE, Vol. 7, No.2 Autumn 2009
Montis, M.; Niehuis, R.; Guidi, M.; Salvadori, S.; Martelli, F.; Stephan, B.:
"Experimental and Numerical Investigation on the Influence of Trailing Edge Bleeding on the Aerodynamics of a NGV Cascade"
GT2009-59910, Proceedings of ASME Turbo Expo 2009: Power for Land, Sea and Air, June 8-12, 2009, Orlando, FL, USA
Muth, B.; Schwarze, M.; Niehuis, R.; Franke, M.:
"Investigation of CFD Prediction Capabilities for Low Reynolds Turbine Aerodynamics"
GT2009-59306, Proceedings of ASME Turbo Expo 2009: Power for Land, Sea and Air, June 8-12, 2009, Orlando, FL, USA
Bindl, S.; Stößel, M.; Niehuis, R.:
"Stall detection within the Low Pressure Compressor of a Twin-Spool Turbofan engine by Tip Flow Analysis"
GT2009-59032, Proceedings of ASME Turbo Expo 2009: Power for Land, Sea and Air, June 8-12, 2009, Orlando, FL, USA
Gomes, R. A.; Niehuis, R.:
"Film Cooling Effectiveness Measurements with Periodic Unsteady Inflow on Highly Loaded Blades with Main Flow Separation"
GT2009-59791, Proceedings of ASME Turbo Expo 2009: Power for Land, Sea and Air, June 8-12, 2009, Orlando, FL, USA
Zachau, U., Niehuis, R., Hoenen, H., Wisler, D.C.:
„Experimental Investigation of the Flow in the Pipe Diffuser of a Centrifugal Compressor Stage under selected Parameter Variations”
ASME paper GT2009-59320, 2009
Montis, M.; Niehuis, R.; Stephan, B.:
"Experimental Investigation of the Influence of Cooling Air Injection on the Aerodynamics of a High Pressure NGV-Cascade"
8th European Conference on Turbomachinery (ETC), Graz, Österreich, 23.-27.3.2009
Gomes, R. A.; Niehuis, R.:
"Film Cooling Effectiveness Measurements on Highly Loaded Blades with Flow Separation"
8th European Conference on Turbomachinery (ETC), Graz, Österreich, 23.-27.3.2009
Schwarze, M.; Martinstetter, M.; Niehuis, R.; Kotzbacher, T.:
"Unsteady Numerical Simulation of the Influence of Periodically Unsteady Wakes on Boundary Layer Development and Loss Behavior of a Highly Loaded Low Pressure Turbine Cascade"
8th European Conference on Turbomachinery (ETC), Graz, Österreich, 23.-27.3.2009
Martinstetter, M.; Niehuis, R.:
"Experimental Investigations on Highly Loaded LP Turbine Cascades"
Vortrag beim VITAL-Workshop "Steps towards clean - quite engines & aircrafts", Budapest, 10. März 2009
Gomes, R. A.:
"Messtechnikimplementierung für aerothermische Untersuchungen am Hochgeschwindigkeits-Gitterwindkanal"
Vortrag beim Seminar für Flugantriebe und Gasturbinen, TU München, Garching,
5. Februar 2009
Emmrich, R., Hönen, H., Niehuis, R.:
„Time Resolved Experimental Investigations of an Axial Compressor with Casing Treatment”,
J. of Turbomachinery, vol. 131, Jan. 2009
2008
2007
"Retrofit of a Digital Engine Control Unit and Integration of an Active Stability Control System"
ISABE-2007-1251, XVIII. ISABE, Bejing, China, 2007
Emmrich, R., Hönen, H., Niehuis, R.:
„Time Resolved Investigations of an Axial Compressor with Casing Treatment Part 1 - Experiment”
ASME paper GT2007-27581, 2007
Emmrich, R., Hönen, H., Niehuis, R.:
„Time Resolved Investigations of an axial Compressor with Casing Treatment Part 2 - Simulation”
ASME paper GT2007-27582, 2007
Wang, Z., Niehuis, R.:
„Assessment of Numerical Methods on a 3.5-stage Axial Compressor”
ISABE-2007-1305, Peking, China, 2007
„Flow Simulation of an Axial Transonic Compressor Stage”
Third Joint HLRB and KONWIHR Result and Reviewing Workshop, 2007
2006
„A Study of nonlinear eddy-viscosity models in a flow solver for turbomachinery”
25th Int. Congress of the Aeronautical Sciences ICAS, Hamburg, 2006
„Unsteady Navier-Stokes Simulation of a Transonic Flutter Cascade Near Stall Conditions Applying Algebraic Transition Models”
J. of Turbomachinery, vol. 128, issue 3, pp. 474-483, 2006
„Clocking Measurements on the 1.5 stage Aachen Cold Air Turbine”
The Seventeenth International Symposium on Transport Phenomena, 4-8 September, Toyama, JAPAN, 2006
OXYCOAL-AC: „Innovative Herausforderung für eine saubere Lösung der zukünftigen Stromversorgung”
VGB PowerTech, 86, (2006) 10, 74/81
"Mapping the Control Parameters of an analog Fuel Control to prepare for the retrofit of a Digital Control Unit"
GT2006-90126, ASME TurboExpo, Barcelona, 2006
"Investigations of the Boundary Layer on a highly loaded Compressor Cascade with wake-induced Trasition"
GT2006-90665, ASME TurboExpo, Barcelona, 2006
"Experimental Investigation of a Generic Compressor Bleed System"
GT2006-90458, ASME TurboExpo, Barcelona, 2006
2005
"Optimale Auslegung von Luftsystemen am Beispiel der Abblase-Konfiguration mehrstufiger Axialverdichter II"
FVV-Informationstagung Turbinen, 28. Sept. 2005, Köln, Heft R532, 2005
"Unsteady Boundary Layer Development due to Wake Passing Effects on a Highly Loaded Linear Compressor Cascade"
AIAA-2005-1054, 17th International Symposium of Airbreathing Engines,
September 4-9 2005, Munich
"Fatal Damage of a Twin-Spool Turbofan Engine due to Fan Blade Off"
AIAA-2005-1206, 17th International Symposium of Airbreathing Engines,
September 4-9 2005, Munich
"Aerodynamic Optimisation of Highly-Loaded HP Turbine Blades for Heavy Duty Gas Turbines"
AIAA-2005-1257, 17th International Symposium of Airbreathing Engines,
September 4-9 2005, Munich
"Aerodynamic Investigations of a Typical Configuration for Bleed Flow in Aeroengines"
AIAA-2005-1264, 17th International Symposium of Airbreathing Engines,
September 4-9 2005, Munich
"Film Cooling of Highly Loaded Blades"
AIAA-2005-1114, 17th International Symposium of Airbreathing Engines,
September 4-9 2005, Munich
"Impact of suction side cooling on the losses of a highly loaded high pressure turbine blade"
6th European Conference on Turbomachinery (ETC 6), 7-11 March 2005, Lille, France
"Aerodynamic optimisation of a HP turbine cascade blade for heavy-duty gas turbine applications"
6th European Conference on Turbomachinery (ETC 6), 7-11 March 2005, Lille, France
2004
"Aero-Thermodynamic Aspects of Film Cooling in Regions of
Separated Flow on the Pressure Side of a High-Lift HPT Blade"
GT-2004-54067, ASME Turbo Expo 2004, June 14-17 2004 Vienna
"Experimentelle Untersuchungen zum Einfluß kombinierter Eintrittstotaldruckstörungen auf das Betriebsverhalten des fünfstufigen Hochdruckverdichters Rig212"
DGLR-2004-122, Jahrbuch 2004, Band I,II
DGLR Jahrestagung 2004, 20./23. September 2004, Dresden
"Einfluss von periodisch instationären Zuströmbedingungen auf das instationäre Grenzschichtverhalten eines hoch belasteten Verdichtergitters."
DGLR-2004-227, Jahrbuch 2004, Band I,II
DGLR Jahrestagung 2004, 20./23. September 2004, Dresden
"Aerodynamische Optimierung hochbelasteter Hochdruckturbinengitter"
DGLR-2004-225, Jahrbuch 2004, Band I, II
DGLR Jahrestagung 2004, 20./23. September 2004, Dresden
Unsteady boundary layer developement due to wake passing effects on a highly loaded linear compressor cascade.
ASME Turbo-Expo Wien, 14.-17. Juni 2004
(published in the "Journal of Turbomachinery", Vol. 126, pp. 493-500, 2004)
"Experimental Operating Range Extension Of A Twin-Spool Turbofan Engine By Active Stability Control Measures"
GT-2004-53077, ASME Turbo Expo 2004, June 14-17, 2004 Vienna
(published as GTP-04-1043 in the "Journal of Engineering for Gas Turbines and Power", Vol. 127, October 2005)
"Surface Roughness Effects on Turbine Blade Aerodynamics",
GT-2004-53314, ASME Turbo Expo 2004, June 14-17 2004 Vienna
(published in the "Journal of Turbomachinery", Vol. 127, Juli 2005)
"Active Stability Control Of The Compression System In A Twin-Spool Turbofan Engine By Air Injection"
ISROMAC 10-2004-073, The 10th of International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, Honolulu, Hawaii, USA, March 07-11, 2004
2003
"Experimentelle Untersuchungen an einem
hochbelasteten Hochdruckturbinengitter ohne
und mit saugseitiger Filmkühlung"
DGLR-2003-201, Jahrbuch 2003, Band III
DGLR Jahrestagung 2003, 17./20. November 2003, München
Untersuchung des Grenzschicht- und Turbulenzverhaltens eines hochbelasteten Transsonik-Verdichtergitters mit Verdichtungsstoß-Grenzschicht-Interaktion.
Deutscher Luft- und Raumfahrtkongress, München, 17.-20. November 2003
Experimental Investigation of Wake-Induced Transition in a Highly Loaded Linear Compressor Cascade
10. ISUAAAT, Durham, NC, USA, 2003
Operational Characteristics of a Twin-spool Turbofan Engine at Inlet Distortions with Reduced Surge Margin
RTO-AVT-2003-029, RTO-AVT-100 Symposium, Warschau, Polen, 2003
Active Stabilization of the Compression System in a Twin-spool Turbofan Engine at Inlet Distortions
ISABE-2003-1083, XVI. ISABE, Cleveland, Ohio, USA, 2003
Numerische Untersuchung des dreidimensionalen Strömungsfeldes eines typischen Abblase-Luftsystems mehrstufiger Axialverdichter
XXXV. Kraftwerktechnisches Kolloquium, Dresden, 2003
Verschiedene Ansätze zur Untersuchung einer typischen Verdichter-Luftabblasung - Nachrechnung experimenteller Ergebnisse
DGLR-Workshop "Luftsysteme in Flugzeugen und Triebwerken", DGLR-Bericht 2003-03, Ottobrunn, 2003
Optimale Abblasekonfigurationen in mehrstufigen Axialverdichter
Abschlussbericht, FVV-Informationtagung Turbinen, Magdeburg, 2003
Doppler Global Velocimetry Messungen in einem Verteilerkanal eines typischen Abblase-Luftsystems in einem mehrstufigen Axialverdichter
GALA Tagung "Lasermethoden in der Strömungsmesstechnik", Braunschweig, 2003
Boundary Layer Investigations in a Highly Loaded Transonic Compressor Cascade with Shock/ Laminar Boundary Layer Interactions
5th European Conference on Turbomachinery, Prag, 2003
2002
Vorderkantenausblasung bei periodisch instationärer Zuströmung
8. Stausseminar der AG TURBO Köln/Deutschland, 2002
Experimentelle Untersuchung zum Einfluß von periodisch instationärer Zuströmung auf das 3D Strömungsfeld einer Film-gekühlten Hochdruckturbinenschaufel
DGLR Paper DGLR-2002-072 , Stuttgart/Deutschland, 2002
Experimental Investigation of turbulence influence of wake passing on the boundary layer developement of highly loaded turbine cascade blades.
Journal of Flow, Turbulence and Combustion, Vol. 69 (3-4), Seiten 229-247, 2002
Aerodynamische Untersuchung eines typischen Abblase-Luftsystems in einem mehrstufigen_Axialverdichters.
DGLR - Jahresband, Teil II, 2002
Experimental investigation of turbulence structures in a highly loaded transonic compressor cascade with schock / laminar boundary layer interactions
5th Symp. on Engineering Turbulence Modelling and Measurements, Mallorca, Spain, 16-18 September 2002
Experimental Investigation of Turbulence Influence of Wake Passing on the Boundary
Layer Development of Higly Loaded Turbine Cascade Blades.
Flow, Turbulence and Combustion, Band 69, Seiten 229–247. Kluwer Academic Publishers, 2002
An Experimental Investigation On The Influence Of Periodic Unsteady Inflow Conditions On Leading Edge Film Cooling
ASME TURBO EXPO 2002, 03. - 06.06.2002
Experiments In Active Stall Control Of A Twin-Spool Turbofan Engine
GT-2002-30002, ASME TURBO EXPO 2002, 03. - 06.06.2002
Influence Of Endwall Contouring On The Transonic Flow In A Compressor Blade
ASME TURBO EXPO 2002, 03. - 06.06.2002
Numerical Investigation Of The Wake-Boundary Layer Interaction On A Higly Loades LP Turbine Cascade Blade
ASME TURBO EXPO 2002, 03. - 06.06.2002
Effects of the Inlet Flow Conditions on the Tip Clearance Flow of an Isolated Rotor
ASME TURBO EXPO 2002, 03. - 06.06.2002
Effects of Riblets on the Loss Behavior of a Highly Loaded Compressor Cascade
ASME TURBO EXPO 2002, 03. - 06.06.2002
Untersuchungen an widerstandsreduzierenden Oberflächenstrukturen für Verdichterbeschaufelungen
Vortrag im Seminar Flugantriebe und Gasturbine, TU München, Garching, 31. Januar 2002, bei Rolly Royce Deutschland am 02.10.02
2001
Einfluß von Ribletstrukturen auf das Verlustverhalten eines aerodynamisch hochbelasteten Verdichtergitters
TU Dresden Conf. Proc. (2001)
Das dynamische Betriebsverhalten eines Turbostrahltriebwerks bei Einlaufstörungen und reduziertem Pumpgrenzabstand
DGLR-Jahrestagung 2001-205 (2001)
Vergleich unterschiedlicher Mehtoden zur Berechnung der Nachlauf/Grenzschicht-Interaktion in einem hoch belasteten Turbinenschaufelgitter
DGLR JT 2001 Hamburg (2001)
Optimization of Three-Dimensionally Designed Turbine Blades and Side Walls
ISABE IS-2001-1058 (2001)
Active Stabilization of a Low Pressure Compressor in a Turbofan Engine with Constant Air Injection
AIAA 2001-3312 (2001)
A Test Case for the numerical Investigation of Wake-Passing Effects on a Highly Loaded LP Turbine Cascade
ASME 2001-GT-0311 (2001)
Effects of Rotating Inlet Distortion on a 5-stage HP Compressor
ASME 2001-GT-0300 (2001)
Experimental Investigation of Heat Transfer in Separated Flow on a Highly Loaded Turbine Cascade
Conf. Proc. of RTO/AVT Symposium 7-11 May 2001 Loen, Norway
Stall Inception in a 5-Stage HP-Compressor under the Influence of Rotating Inlet Distortion
Conf. Proc. of 4th European Conference on Turbomachinery, 20-23 March 2001, Florence, Italy (2001)
2000
Vorderkantenausblasung bei periodisch instationärer Zuströmung
7. Statusseminar AG TURBO DLR Köln (2000)
Hochbelastete ungekühlte Turbinenbeschaufelung
7. Statusseminar AG TURBO DLR Köln (2000)
Seitenwandkonturierung in Turbinengittern
7. Statusseminar AG TURBO DLR Köln (2000)
Glue-On Hot Film Sensors to Investigate Heat Transfer on a Highly Loaded LP Film-Cooled Turbine Blade
15th Symposium on Measuring Techniques for Transonic and Supersonic Flow in Cascades and Turbomachines, Florenz, Sep-tember 2000
A Coupled Steady-Unsteady-State Data Acquisition System for the Investigation of Rotating Inlet Distortions at a Multi-Stage Compressor Test Facility
15th Symposium on Measuring Techniques for Transonic and Supersonic Flow in Cascades and Turbomachines, Florenz, September 2000
Fast Response Pressure Transducers for the Investigation of Wake-Induced Transition on a Highly Loaded LP Turbine
15th Symposium on Measuring Techniques for Transonic and Supersonic Flow in Cascades and Turbomachines, Florenz, September 2000
Numerische Simulation eines filmgekühlten Turbinengitters mit einer Variation der Ausblasebohrungen
DGLR Jahrestagung 2000, Leipzig
Einfluss widerstandsreduzierender Oberflächenstrukturen auf das Verlustverhalten eines aerodynamisch hochbelasteten Verdichtergitters
DGLR Jahrestagung 2000, Leipzig
Experimental and Numerical Investigations of the Flow Behaviour in Compressor Cascades under the Influence of Wakes
9th Int. Symp. on Unsteady Aerodynamics and Aeroelasticity of Turbomachines, Lyon, France (2000)
A Presentation of Detailed Experimental Data of a Suction Siede Film Cooled Turbine Cascade
ASME 2000-GT-0296 (2000)
Comparison of Two Highly Loaded Low Pressure Turbine Cascades Under the Influence of Wake-Induced Transition
ASME 2000-GT-268 (2000)
Experimental and Numerical Investigation of Wake-Induced Transition on a Highly Loaded LP Turbine Cascade at Low Reynolds Numbers
ASME 2000-GT-0269 (2000)
Steady Performance Measurements of a Turbofan Engine with Inlet Distortions Containing Co- and Counter-Rotating Swirl from an Intake Diffuser for Hypersonic Flight
ASME 2000-GT-0011 (2000)
Systematic Experimental an Numerical Investigations on the Aerothermodynamics of a Film Cooled Turbine Cascade with Variation of the Cooling Hole Shape - Part II: Numerical Approach
ASME 2000-GT-0298 (2000)
Systematic Experimental an Numerical Investigations on the Aerothermodynamics of a Film Cooled Turbine Cascade with Variation of the Cooling Hole Shape - Part I: Experimental Approach
ASME 2000-GT-0295 (2000)
Turbulence Structures of Leading Edge Film Cooling Jets
ASME 2000-GT-0255 (2000)
The Influence of Multimode Transition Initiated by Periodic Wakes on the Profile Loss of a Linear Compressor Cascade
ASME 2000-GT-0271 (2000)
The Use of Hot-Wire Anemometry to Investigate Unsteady Wake-Induced Boundary-Layer Development on a High Lift LP Turbine Cascade
ASME 2000-GT-0049 (2000)
The Influence of Transient Inlet Distortions on the Instability Inception of a Low Pressure Compressor in a Turbofan Engine
ASME 2000-GT-0505 (2000)
Investigations of Wake-Induced Transition on the LPT Cascades T106A-EIZ and T106D-EIZ
ERCOFTAC Workshop 19-23 March 2000, La Clusaz (2000)
Investigations of the Aerodynamics and the Heat Transfer on the Suction Side of the Film Cooled Turbine Cascade T106-300
ERCOFTAC Workshop 19-23 March 2000, la Clusaz (2000)
Verfahren zur Früherkennung von Verdichterinstabilitäten am Beispiel des ND-Verdichters eines Turbofan-Triebwerks
DGLR-Fachausschuß-Sitzung RWTH Aachen, 2000
1999 und früher
Turbomachichery Research at the Jet Propulsion Institute of the University of the Federal Armed Forces Munich
ERCOFTAC Bulletin No. 42,(1999), pp 19-30
Numerical Simulation of Flow Instabilities in High Speed Multistage Compressors
Journ. of Thermal Science Vol. 8, No. 1, pp 23-31 (1999)
Untersuchungen zum Einfluß der Rotor/Stator-Interaktion auf die saugseitige Transition eines hochbelasteten ungekühlten Niederdruck-Turbinengitters
DGLR Jahrestagung 1999, Berlin
Performance of a Turbofan Engine with Inlet Distortions from the Intake Diffuser of a Combined Cycle Engine for Hypersonic Flight
ISABE Paper IS-7076, Florenz, Italy (1999)
The Influence of Technical Surface Roughness of Modern Blade Manufacturing Methods on the Flow Around a Compressor Cascade
ISABE Paper IS-7019, Florenz, Italy (1999)
Experimental Investigation of Wake-Induced Transition in a Linear Compressor Cascade with Controlled Diffusion Blading
ISABE Paper IS-7057, Florenz, Italy (1999)
The Secondary Flow Field of a Turbine Cascade with 3D Airfoil Design and Endwall Contouring at Off-Design Incidence
ASME 99-GT-211 (1999)
Film Cooling Over a Concave Surface Through a Row of Expanded Holes
ASME 99-GT-039 (1999)
Stall Inception in a 5 stage HP Compressor with Increased Load Due to Inlet Distortion
ASME 99-GT-440 (1999)
The Influence of Technical Surface Roughness on the Flow around a Highly Loaded Compressor Cascade
ASME 99-GT-366 (1999)
Journal of Turbomachinery Vol. 122 No. 3 416-425
Model Wind-Tunnel Tests for the Optimisation of the Flow Field inside the Subsonic Diffuser of an Intake for a Combined Cycle Engine for Hypersonic Flight
Conference Proceedings of the 1999 European Propulsion Forum, Pau, France, (1999)
Proposal for a New ERCOFTAC Test Case: Leading Edge Film Cooling on a Large High Pressure Turbine Cascade
ERCOFTAC Workshop 04-07 January 1999, Aussois (1999)
Optimierung hochbelasteter Turbinen- und Verdichterbeschaufelungen mit Berücksichtigung instationärer Zuströmung
6. Statusseminar AG TURBO DLR Köln (1998)
Investigation of Wake-Induced Transition on a Highly Loaded Low Pressure Turbine Cascade
Conf. Proc. of 3nd European Conference on Turbomachinery, 2-5 March 1999 C557/068/99, London, UK (1999)
Experimentelle Untersuchung zum Transitionsverhalten in Verdichtergittern mit periodisch veränderlicher Zuströmung
STAB Fachsymposium Berlin, 1998
Untersuchungen des Wärmeübergangs an einem filmgekühlten Turbinengitter im Hochgeschwindigkeits-Gitterwindkanal
DGLR Jahrestagung 1998, Bremen
Numerical Investigations of the Flow Field Inside the Intake Diffuser of a Combined Cycle Engine for Hypersonic Flight
4th ECCOMAS Computational Fluid Dynamics Conference, Athens, September 1998
A Measurement Technique to Investigate the Influence of Surface Roughness on the Flow around a Highly Loaded Compressor Cascade
14th Symposium on Measuring Techniques for Transonic and Su-personic Flow in Cascades and Turbomachines, Limerick, September 1998
The Use of Simultaneous Surface Hot Film Anemometry to Investigate Unsteady Wake Induced Transition in Turbine and Compressor Cascades
14th Symposium on Measuring Techniques for Transonic and Su-personic Flow in Cascades and Turbomachines, Limerick, September 1998
Stall Inception in the Compressor System of a Turbofan Engine
ASME 98-GT-475 (1998)
A Numerical Study of the Influence of Grid Refinement and Turbulence Modelling on the Flow Field inside a Highly Loaded Turbine Cascade
ASME 98-GT-240 (1998)
Controlling the Secondary Flow in a Turbine Cascade by 3D Airfoil Design and Endwall Contouring
ASME 98-GT-072 (1998)
Experimental and Numerical Investigations of Flapping Wing Propulsion and its Application for Boundary-Layer Control
ASME 98-GT-046 (1998)
A Systematic Experimental Study on the Aerodynamics of Leading Edge Film Cooling on a Large Scale High Pressure Turbine Cascade
ASME 98-GT-434 (1998)
Rotating Stall Inception with Inlet Distortion in the Low Pressure Compressor of a Turbofan Engine
19th Int. Symp. Aircraft Integrated Monitoring Systems, May 1998 Garmisch-Partenkirchen (1998)
Experimental Set-Up, Measurement and Analysis of the Onset of Compressor Flow Instabilities in an Aero Engine
17th Int. Congr. on Instrumentation in Aerospace Simulation Facilities, Monterey, USA (1997)
Set-Up of a Heat Transfer Coefficient Measurement System at the High Speed Cascade Wind Tunnel
Eurotherm Seminar No. 55 on "Heat Transfer in Single Phase Flows", Santorin, Greece (1997)
An Experimental Flow Investigation of an HP Five-Stage Compressor Exhibiting Rotating Stall due to Distorted Inlet Flow Conditions
8th Int. Symp. on Unsteady Aerodynamics and Aeroelasticity of Turbomachines, Stockholm, Sweden (1997)
Investigation of the Boundary Layer Development on a Highly Loaded Low Pressure Turbine Cascade under the Influence of Unsteady Flow Conditions
8th Int. Symp. on Unsteady Aerodynamics and Aeroelasticity of Turbomachines, Stockholm, Sweden (1997)
Experimental and Numerical Investigations of the Influence of Endwall-Inclination and Contouring on the Flow Field in a Highly Loaded Turbine Cascade
ISABE Chattanooga, USA (1997)
The Influence of Slot Ejection and Showerhead Ejection on the 3D Flowfield of a Film-Cooled Turbine Blade under Consideration of Side Wall Effects
ISABE Chattanooga, USA (1997)
Flow Field Measurements on a Large Scale Turbine Cascade with Leading Edge Film Cooling by Two Rows of Holes
ASME 97-GT-524 (1997)
Design of Aero Engines for Safety, Reliability, Maintainability and Cost
Conference Proceedings of the 1997 European Propulsion Conference, Berlin, (1997)
Influence of Taper, Reynolds Number and Mach Number on the Secondary Flow of a Highly Loaded Turbine Cascade
Conf. Proc. of 2nd European Conference on Turbomachinery,
5-7 March, Antwerpen (1997)
Numerical Simulation of Active Suppression of Rotating Stall in Axial Compression Systems
Journ. of Thermal Science Vol. 5, No. 4, pp 231-242 (1996)
Messungen an einer filmgekühlten Turbinenschaufelvorderkante
5. Statusseminar AG TURBO DLR Köln (1996)
Messungen an einer filmgekühlten Turbinenschaufelvorderkante
5. Statusseminar AG TURBO DLR Köln (1996)
Numerische Untersuchung der Strömung in einem hochbelasteten Axialverdichter mit unterschiedlichen 3D Navier-Stokes Verfahren
DGLR Jahrestagung Dresden (1996)
A New Multi-Stage Compressor Test Facility for Inlet Distortion Investigations
13th Symposium on Measuring Techniques for Transonic and Supersonic Flow in Cascades and Turbomachines, Zürich, September 1996
WINPANDA - An Enhanced PC-Based Data Acquisition System for Wake and Profile Pressure Distribution Measurements at the High Speed Cascade Wind Tunnel
13th Symposium on Measuring Techniques for Transonic and Supersonic Flow in Cascades and Turbomachines, Zürich, September 1996
The Generation of Instationary Flow Conditions in the High Speed Cascade Wind Tunnel
13th Symposium on Measuring Techniques for Transonic and Supersonic Flow in Cascades and Turbomachines, Zürich, September 1996
Influence of Tip Clearance, Aspect Ratio, Blade Loading and Inlet Boundary Layer on Secondary Losses in Compressor Cascades
ASME 96-GT-505 (1996)
Experimental Investigation of Turbulence Structures in the Boundary Layer of a Highly Loaded Turbine Cascade
ASME 96-GT-249 (1996)
Durham Low Speed Turbine Cascade - Test Case 3
ERCOFTAC Workshop 08-11 January 1996, Courchevel (1996)
Numerical and Experimental Investigations of the Flow Field Inside the Intake Duct of a Combined Cycle Engine for Hypersonic Flight
Proc. of ASME Conf. on "Computational Fluid Dynamics in Aeropropulsion", San Francisco (1995)
Numerische und experimentelle Untersuchung des Strömungsfeldes im Einlaufkanal eines Hyperschall-Kombinationstriebwerks
DGLR Jahrestagung Bonn DGLR-JT95-072 (1995)
Transient Performance of Turbofan Engines with Respect to Unsteady Compressor Flow near the Stability Limit
ISABE Melbourne (1995)
Numerical and Experimental Investigations of Film Cooling from a Row of Holes at the Suction Side of a Highly Loaded Turbine Blade
ISABE Melbourne (1995)
Strömungssichtbarmachung und Untersuchungen zum Verlustverhalten an einem Turbinenschaufelgitter mit Vorderkanten-Fimkühlung
DGLR FA TU Berlin (1995)
Mischungsvorgänge zwischen Kühlfilmen und Gitterströmung an einem hochbelasteten Turbinengitter
DGLR FA TU Berlin (1995)
Calculations of Effects of Rotating Inlet Distortion on Flow Instabilities in Compression Systems
ASME 95-GT-196 (1995)
Experimental Investigation of Boundary Layer Transition and Turbulence Structures on a Highly Loaded Compressor Cascade
ASME 95-GT-129 (1995)
Investigations of Shock/Boundary-Layer Interaction in a Highly Loaded Compressor Cascade
ASME 95-GT-84 (1995)
The Effect of Incoming Wakes on Boundary Layer Transition of a Highly Loaded Turbine Cascade
AGARD CP 571 (1995)
Schlieren Method with Quantitative Evaluation by Digital Image Processing
12th Symposium on Measuring Techniques for Transonic and Supersonic Flow in Cascades and Turbomachines, Prague, September 1994
The Generation of Isotropic Turbulence in the High Speed Cascade Wind Tunnel
12th Symposium on Measuring Techniques for Transonic and Supersonic Flow in Cascades and Turbomachines, Prague, September 1994
Improved Blade Profile Loss and Deviation Angle Models for Advanced Transonic Compressor Bladings
Part II: A Model for Supersonic Flow
ASME 94-GT-336 (1994)
Improved Blade Profile Loss and Deviation Angle Models for Advanced Transonic Compressor Bladings
Part I: A Model for Subsonic Flow
ASME 94-GT-335 (1994)
The Aerodynamic Mixing Effect of Discrete Cooling Jets with Mainstream Flow on a Highly Loaded Turbine Blade
ASME 94-GT-235 (1994)
Journ. of Turbomachinery Vol. 118 No. 3 (1996) pp 468-478
Durham Low Speed Turbine Cascade - 3D-Navier-Stokes Calculation
ERCOFTAC Workshop 10-13 January 1994, Val d'Isere (1994)
Einfluß kombinierter Drall- und Totaldruck-Eintrittsstörungen auf das Stabilitätsverhalten von Turbostrahltriebwerken
DGLR Jahrestagung Göttingen DGLR-JT93-047 (1993)
A System for Monitoring, Measurement and Analysis of Transient Performance and Stall Phenomena of Gas Turbine Engines
Conf.Proc. Instrumentation in Aerospace Facilities, Saint-Louis (1993)
Experimental Investigations of the Influence of Incoming Wakes on the Losses of a Linear Turbine Cascade
ASME 93-GT-394 (1993)
Highly Loaded Tandem Compressor Cascade with Variable Camber and Stagger
ASME 93-GT-235 (1993)
The Influence of Load Distribution on Secondary Flow in Straight Turbine Cascades
ASME 93-GT-86 (1993)
Journ. of Turbomachinery Vol. 117 No. 1 (1995) pp 133-141
Analysis of Cooling Jets near the Leading Edge of Turbine Blades
AGARD CP 534 (1993)
Die Auswirkungen unterschiedlicher Belastungsverteilungen von Turbinengittern auf die Energiedissipation und auf die Verteilung der Verluste und des Abströmwinkels über der Schaufelhöhe
DGLR-Fachausschuß-Sitzung Uni Stuttgart, 1993
Measuring Techniques for Transonic and Supersonic Flow in Cascades and Turbomachines
Conference Proceedings, Neubiberg, 1993
The Aerodynamic Effect of Coolant Ejection in the Leading Edge Region of a Film Cooled Turbine Blade
AGARD CP 527 (1992)
The Experimental Set-Up of a Triple-Sensor Anemometry and its Controlling System at the High-Speed Cascade Wind Tunnel
11th Symposium on Measuring Techniques for Transonic and Supersonic Flow in Cascades and Turbomachines, Neubiberg, September 1992
Steady and Transient Perfomarmance Prediction of Gas Turbine Engines
AGARD LS 183 (1992)
Bestimmung der wesentlichen Einflußgrößen in der Korrelation der Sekundärströmungsverluste bei Veränderung des Schaufelseitenverhältnisses
MTZ 53, Heft 6 (1992)
The Influence of Intake Swirl Distortion on the Steady-State Performance of a Low Bypass, Twin-Spool Engine
AGARD CP-498 (1991)
Experimental Analysis of the Dynamic Performance of Turbojet Engines
ISABE Nottingham (1991)
Performance Improvements of Compressor Cascades by Controlling the Profile and Sidewall Boundary-Layers
ASME 91-GT-260 (1991)
Bestimmung der wesentlichen Einflußgrößen in der Korrelation der Sekundärströmungsverluste bei Veränderung des Schaufelseitenverhältnisses
FVV Heft R 482 (1991)
PANDA - A new Data Acquisition System for Wake and Profile Pressure Distribution Measurements at the High-Speed Cascade Wind Tunnel
10th Symposium on Measuring Techniques for Transonic and Supersonic Flows in Cascades and Turbomachines, Brussel, September 1990
The Influence of Inlet Swirl Distortions on the Performance of a Jet Propulsion Two-Stage Axial Compressor
ASME 90-GT-147 (1990)
Test Cases for Computation of Internal Flows in Aero Engine Components
AGARD-AR-275 (1990)
Overview on Test Cases for Computation of Internal Flows in Turbomachines
ASME 89-GT-46 (1989)
Review of Turbomachinery Blading Design Problems
AGARD-LS-167 (1989)
Blading Design for Axial Turbomachines
AGARD-LS-167 (1989)
Measuring Techniques at the High-Speed Cascade Windtunnel of the University of the Federal Armed Forces Munich
9th Symposium on Measuring Techniques for Transonic and Supersonic Flows in Cascades and Turbomachines, Oxford, March 1988
Development of Intake Swirl Generators for Turbo Jet Engine Testing
AGARD-CP-400 (1986)
Influence of Free Stream Turbulence and Blade Pressure Gradient on Boundary-Layer and Loss Behaviour of Turbine Cascades
ASME 86-GT-234 (1986)
Evaluation of the Blade-to-Blade Flow from a High-Speed Compressor Rotor
ASME 86-GT-117 (1986)
The High-Speed Cascade Wind Tunnel of the German Armed Forces University Munich
8th Symposium on Measuring Techniques for Transonic and Supersonic Flows in Cascades and Turbomachines, Genua, Oct. 1985
Advanced Design Concepts for Axial Compressors and Axial Turbines
Concepts 85. Conf. Proc. (1985)
Überblick über neue Beschaufelungskonzepte
DGLR FA Antriebe (1984)
New Design Concepts for Bladings of Axial Turbomachines
15th ICAS Conf. Proc. (1983)
Design of Transonic Compressor Cascades for Minimal Shock Losses and Comparison with Test Results
AGARD Conf. Proc. CP 351 (1983)
Survey on the Effects of Blade Surface Roughness on Compressor Performance
AGARD AR 175 (1982)
Survey of Models for Shock and Shock/Boundary-Layer Interaction Loss Prediction
AGARD AR 175 (1982)
Advanced Concepts in Turbomachinery
Lecture Series at the Fluid Dynamic Institute of Dartmouth College, Hanover, N.H. August, 17-21, 1981
Vorausberechnung des Betriebsverhaltens von transsonischen Axialverdichtern
FVV-Kurzinformation 63/80 (1980)
Theoretical and Experimental Investigations on Aerodynamically Highly-Loaded Compressor Bladings with Boundary-Layer Control
ISABE Orlando, USA (1979)
Aerodynamisch hochbelastete Verdichterbeschaufelung mit Grenzschichtbeeinflussung
Forschungsbericht aus der Wehrtechnik BMVg FBWT 77-4 (1977)
Auslegungsgrundlagen für transsonische Axialverdichter
FVV-Kurzinformation
73/76 (1976)
Aerodynamische Entwicklung eines dreistufigen Transonik-Frontgebläses
ZfW 22 (1974), Heft 4, S. 135-144
Semi-Empirical Methods for Transonic Flow in Turbomachinery
Lecture at VKI short course "Transonic Flow in Turbomachinery"
VKI LS 59 (1973), Brüssel
Analytical Approach for the Loss and Deflection Behaviour of Cascades in Transonic Flow Including Axial Mass Flow Variation
AGARDograph No. 164 (1972)
Ein Verfahren zum Bestimmen der verlustbehafteten transsonischen Schaufelgitterströmung bei vorgegebener Druckverteilung
Forschg.Ing.Wes. 38 (1972) Nr. 3, S. 69 - 81
Ein halbempirisches Verfahren zum Bestimmen der reibungsbehafteten transsonischen Schaufelgitterströmung mit Einschluß von Überschallfeldern und Verdichtungsstößen
Dissertation TU München (1970)
Kurzfassung in Forschg. Ing.Wes 36 (1970) Nr.4, S.101-110
A Semi-Empirical Approach of the Transonic Flow Past Cascades Including Shock and Viscous Effects
AGARD Conf. Proc. No. 34 (1968)
PhD Thesises
2021
Rademakers, R.P.M.: "On Intake-Compressor Interactions within Integrated Propulsion Systems
UniBw München (Niehuis, Schiffer), Prüfung: 29.07.2021
2020
Kächele, T.: "Numerische Untersuchung der Interaktionsphänomene in einer Konfiguration bestehend aus kompaktem Einlauf und Triebwerksverdichter"
UniBw München (Niehuis, Friedrichs), Prüfung: 09.10.2020
2018 - 2016
2018
Händel, D.: Experimentelle Untersuchung und Weiterentwicklung eines variablen Eintrittsleitapparates für die Vordrallregelung in Turbomaschinen
UniBW München (Niehuis, Seume), Prüfung: 12.07.2018
Montis, M.: Aerodynamics Effects of Coolant Ejections in a High-Pressure Gas Turbine Airfoil
UniBW München (Niehuis, Martelli), Prüfung: 03.07.2018
Stotz, S.: Experimentelle Untersuchung druckseitiger Ablösemechanismen an Niederdruckturbinenprofilen
UniBW München (Niehuis, Heitmeir), Prüfung: 25.05.2018
2017
Ciorciari, R.: Analysis of Unsteady Secondary Flows in Linear Low-Pressure Turbine Cascades
UniBW München (Niehuis, Vogeler), Prüfung: 15.12.2017
Stößel, M.: Umsetzung und Erprobung eines Ejektor-Einblasesystems zur Stabilisierung des Niederdruckverdichters am Turbostrahltriebwerk Larzac 04
UniBW München (Niehuis, Gümmer), Prüfung: 01.12.2017
Brachmanski, R.: Niederdruckturbinenprofile unter dem Einfluss hoher Turbulenzgrade
UniBW München (Niehuis, Seume), Prüfung: 14.07.2017
2015 - 2011
2014
Lesser, A.: Numerische Untersuchungen von Axialverdichtern mit gestörter Zuströmung
UniBW München (Niehuis, Friedrichs), Prüfung: 24.10.2014
Brandt, H.: Numerische Untersuchung turbulenter, dreidimensionaler Strömungen in Aus- und Abblasesystemen von Turbomaschinen
UniBW München (Niehuis, Pfitzner), Prüfung: 28.03.2014
2012
Muth, B.: Einfluss kleiner Reynolds-Zahlen auf das Verlust- und
Umlenkverhalten von Niederdruckturbinengittern
UniBW München (Niehuis, Peitsch), Prüfung: 09.03.2012
Schwarze, M.: Numerische Simulation hochbelasteter Niederdruckturbinen unter besonderer Berücksichtigung periodisch instationärer Zuströmung
UniBW München (Niehuis, Peitsch), Prüfung: 23.02.2012
2011
Iseler, J.: Numerische Untersuchung des instationären Strömungs- und Leistungsverhalten von Verdichterbeschaufelungen bei homogener und gestörter Zuströmung
UniBW München (Niehuis, Pfitzner), Prüfung: 22.07.2011
Ludewig, T.: Applikation aktiver und semiaktiver Methoden der Grenzschichtbeeinflussung an modernen hochbelasteten Niederdruckturbinen-Beschaufelungen
UniBW München (Niehuis, Kosyna), Prüfung: 18.02.2011
2010 und früher
2010
Gomes, R. A.: On Aerothermal Effects of Film Cooling on Turbine Blades with Flow Separation
UniBw München (Niehuis, Hennecke), Prüfung: 25.06.2010
Bindl, S.: Realisierung einer autarken Applikation zur Erkennung und Unterdrückung von Verdichterinstabilitäten am Turbostrahltriebwerk Larzac 04
UniBw München (Niehuis, Schiffer), Prüfung: 29.04.2010
Martinstetter, M.:
Experimentelle Untersuchungen zur Aerodynamik hoch belasteter Niederdruckturbinen-Beschaufelungen
UniBW München (Niehuis, Heitmeir), Prüfung: 23.4.2010
2007
Homeier, L.
Experimentelle Untersuchungen an hochbelasteten Hochdruckturbinengittern mit Filmkühlausblasung in Gebieten mit positivem Druckgradienten
UniBw München (Niehuis, Schiffer), Prüfung: 20.04.2007
2006
Hilgenfeld, L.
Turbulenzstrukturen in hochbelasteten Transsonik-Verdichtergittern unter besonderer Berücksichtigung der Verdichtungsstoß-Grenzschicht-Interferenz
UniBw München (Pfitzner, Niehuis), Prüfung: 17.11.2006
Cardamone, P.
Aerodynamic Optimisation of Highly Loaded Turbine Cascade Blades for Heavy Duty Gas Turbine Applications
UniBw München (Pfitzner, Martelli), Prüfung: 03.02.2006
2005
Reuss, N.
Untersuchung von kombinierten Eintrittstotaldruckstörungen auf das instationäre Betriebsverhalten eines mehrstufigen Hochdruckverdichters
UniBw München (Mundt, Staudacher), Prüfung: 18.11.2005
Schwarz, C.
Aerodynamische Untersuchungen an Abblase-Luftsystemen mehrstufiger Axialverdichter
UniBw München (Pfitzner, Bauer), Prüfung: 21.10.2005
Scheidler, S. G.
Untersuchung der systemaspekte stabilitätsverbessernder Maßnahmen in Gasturbinen
UniBw München (Mundt, Hennecke), Prüfung: 14.10.2005
2004
Nagel, M. G.
Numerische Optimierung dreidimensional parametrisierter Turbinenschaufeln mit umfangsunsymmetrischen Plattformen
UniBw München (Pfitzner, Lawerenz), Prüfung: 14.09.2004
Peters, T.
Untersuchung von Strömungsinstabilitäten in einem mehrstufigen Axialverdichter unter dem Einfluss rotierender Eintrittsstörungen
UniBw München (Mundt, Fiedler), Prüfung: 09.01.2004
2003
Wolff, S.
Aerodynamische Effekte bei Vorderkanten-Filmkühlausblasung an hochbelasteten Turbinengittern unter dem Einfluss periodisch instationärer Zuströmung
UniBw München (Pfitzner, Koschel), Prüfung: 21.11.2003
Boese, M.
Einfluß widerstandsreduzierender Oberflächenstrukturen auf das Strömungsverhalten eines hochbelasteten Verdichtergitters
UniBw München (Mundt, Vollheim), Prüfung: 31.10.2003
Leinhos, D.
Aktive Stabilisierung der Verdichterströmung in einem Zweikreis-Turbostrahltriebwerk
UniBw München (Mundt, Hennecke), Prüfung: 13.01.2003
2002
Kampitsch, M.
Numerische Untersuchung der instationären Nachlauf/Grenzschicht-Interaktion in Turbinen- und Verdichterschaufelgittern und Vergleich mit Messungen
UniBw München (Pfitzner, Kau), Prüfung: 19.11.2002
Stadtmüller, P.
Grenzschichtentwicklung und Verlustverhalten von hochbelasteten Turbinengittern unter dem Einfluß periodisch instationärer Zuströmung
UniBw München (Mundt, Hourmouziadis), Prüfung: 05.08.2002
2001
Teusch, R.
Der Einfluß periodisch instationärer Zuströmung auf das Transitionsverhalten von Verdichtergittern
UniBw München (Fottner, Fiedler), Prüfung: 26.01.2001
2000
Brunner, St.
Untersuchung des Strömungsverhaltens von hochbelasteten ungekühlten Niederdruck-Turbinengittern unter Berücksichtigung der Rotor-Stator Interaktion
UniBw München (Fottner, Niehuis), Prüfung: 20.11.2000
Schmid, N.
Leistungsverhalten von Turbostrahltriebwerken unter dem Einfluß von Hyperschallflug-typischen Eintrittsstörungen
UniBw München (Fottner, Rick), Prüfung: 08.08.2000
Ganzert, W.
Untersuchungen zur Optimierung der Kühlluft-Ausblasekonfigurationen fortschrittlicher Turbinenbeschaufelungen
UniBw München (Fottner, Hennecke), Prüfung: 03.08.2000
Leipold, R.
Einfluß der durch moderne Herstellungsverfahren erzeugten Oberflächenrauhigkeiten auf das Strömungsverhalten von Verdichtergittern
UniBw München (Fottner, Adam), Prüfung: 28.01.2000
1999
Bernhard, D.
Untersuchungen zum Einfluß kombinierter Drall- und Totaldruck-Eintrittsstörungen auf das Stabilitätsverhalten von Turbostrahltriebwerken
UniBw München (Fottner, Rick), Prüfung: 11.10.1999
Duden, A.
Strömungsbeeinflussung zur Reduzierung der Sekundärströmungen in Turbinengittern
UniBw München (Fottner, Broichhausen), Prüfung: 22.01.1999
1998
Höss, B.
Zum Einfluß von Eintrittsstörungen auf das dynamische Leistungsverhalten von Turbostrahltriebwerken unter besonderer Berücksichtigung instabiler Verdichterströmungen
UniBw München (Fottner, Rick), Prüfung: 22.12.1998
Ardey, S.
Untersuchung der aerodynamischen Effekte von Vorderkanten-Kühlluftausblasung an einem hochbelasteten Turbinengitter
UniBw München (Fottner, Hennecke), Prüfung: 10.06.1998
Dohring, Cl.
Der Schub des schlagenden Flügels und seine Anwendung zur Grenzschichtbeeinflussung - eine experimentelle und numerische Untersuchungen
UniBw München (Fottner, Platzer), Prüfung: 28.05.1998
Jahnen, W.
Untersuchung von Strömungsinstabilitäten in einem mehrstufigen Axialverdichter unter dem Einfluß von Eintrittsstörungen
UniBw München (Fottner, Fiedler), Prüfung: 27.02.1998
Acton, P.
Untersuchung des Grenzschichtumschlages an einem hochbelasteten Turbinengitter unter inhomogenen und instationären Zuströmbedingungen
UniBw München (Fottner, Hennecke), Prüfung: 16.02.1998
Hildebrandt, Th.
Weiterentwicklung von 3D Navier-Stokes-Strömungsrechenverfahren zur Anwendung in hochbelasteten Verdichter- und Turbinengittern
UniBw München (Fottner, Lawerenz), Prüfung: 30.01.1998
1997
Schnaus, J.
Untersuchung zum Einfluß der Seitenwandneigung und Seitenwandkonturierung auf das Strömungsverhalten von hochbelasteten Turbinengittern
UniBw München (Fottner, Wagner), Prüfung: 04.08.1997
1996
Engber, M.
Untersuchung von Ablöseblasen in Turbinen- und Verdichtergittern unter dem Einfluß einer inhomogenen Zuströmung
UniBw München (Fottner, Vollheim), Prüfung: 09.12.1996
Müller, J.-E.
Numerische und experimentelle Untersuchung des Strömungsfeldes im Einlaufkanal eines Hyperschall-Kombinationstriebwerks
UniBw München (Fottner, Rick), Prüfung: 18.09.1996
Hübner, J.
Experimentelle und theoretische Untersuchung der wesentlichen Einflußfaktoren auf die Spalt- und Sekundärströmung in Verdichtergittern
UniBw München (Fottner, Stark), Prüfung: 09.08.1996
Sachmann, J.
Experimentelle und numerische Untersuchungen an einem Tandem-Verdichtergitter mit adaptiver Staffelung und Wölbung
UniBw München (Fottner, Gallus), Prüfung: 02.04.1996
1995
Herpel, Th.
Untersuchungen zum dynamischen Leistungsverhalten von Turbostrahltriebwerken unter Berücksichtigung instationärer Verdichterströmungen nahe der Stabilitätsgrenze
UniBw München (Fottner, Fiedler), Prüfung: 23.11.1995
Wunderwald, D.
Untersuchung der Turbulenzstrukturen in hochbelasteten Verdichter- und Turbinengittern
UniBw München (Fottner, Hennecke), Prüfung: 10.11.1995
Bell, R.
Untersuchungen zur Stoß/Grenzschicht-Interferenz an aerodynamisch hochbelasteten Transsonik-Verdichtergittern
UniBw München (Fottner, Wagner), Prüfung: 12.07.1995
1994
Wilfert, G.
Experimentelle und numerische Untersuchungen der Mischungsvorgänge zwischen Kühlfilmen und Gitterströmung an einem hochbelasteten Turbinengitter
UniBw München (Fottner, Koschel), Prüfung: 13.09.1994
1993
Weiß, A.
Der Einfluß der Profilgeometrie auf die Entwicklung der Sekundärströmung in Turbinengittern
UniBw München (Fottner, Broichhausen), Prüfung: 06.08.1993
1992
Beeck, A.
Strömungsfelduntersuchungen zum aerodynamischen Verhalten eines hochbelasteten Turbinengitters mit Kühlluftausblasung an der Schaufelvorderkante
UniBw München (Fottner, Hennecke), Prüfung: 28.10.1992
1991
Ladwig, M.
Experimentelle Untersuchungen zum Einfluß einer inhomogenen Zuströmung auf die Entwicklung des Strömungsfeldes in Turbinenschaufelgittern
UniBw München (Fottner, Koschel), Prüfung: 19.12.1991
Pazur, W.
Experimentelle und numerische Untersuchungen zum Einfluß von Eintrittsdrallstörungen auf das Betriebsverhalten von Flugtriebwerksverdichtern
UniBw München (Fottner, Fiedler), Prüfung: 30.07.1991
Watzlawick, R.
Untersuchung der wesentlichen Einflußgrößen auf die Sekundärverluste in Verdichter- und Turbinengittern bei Variation des Schaufelseitenverhältnisses
UniBw München (Fottner, Grahl), Prüfung: 02.05.1991
Berns, W.
Untersuchungen zur experimentellen Analyse des dynamischen Leistungsverhaltens von Turbostrahltriebwerken
UniBw München (Fottner, Koschel), Prüfung: 26.04.1991
1990
Römer, N.
Theoretische und experimentelle Untersuchungen zum Umschlagverhalten der Profilgrenzschicht an Verdichter- und Turbinengittern
UniBw München (Fottner, Römer), Prüfung: 01.02.1990
Scheugenpflug, H.
Theoretische und experimentelle Untersuchungen zur Reduzierung der Randzonenverluste hochbelasteter Axialverdichter durch Grenzschichtbeeinflussung
UniBw München (Fottner, Grahl), Prüfung: 18.01.1990
1988
Meyer, W.
Untersuchungen zum Einfluß von Einlaufdrallstörungen auf das stationäre Betriebsverhalten von Turbostrahltriebwerken
UniBw München (Fottner, Fiedler), Prüfung: 09.12.1988
Sturm, W.
Theoretische und experimentelle Untersuchungen zum Einsatz der Ausblasung als Mittel zur aktiven Beeinflussung der Profilgrenzschicht in hochbelasteten Verzögerungsgittern
UniBw München (Fottner, Kappler), Prüfung: 25.11.1988
1987
Neuhoff, F.
Entwicklung und Anwendung einer Meßtechnik zur Bestimmung der Strömungsgrößen und der Verluste eines Verdichter-Rotors bei hoher subsonischer und transsonischer Anströmung
UniBw München (Fottner, Gallus), Prüfung: 26.06.1987
Neunert, P.
Theoretische und experimentelle Untersuchungen zur Vorgabe einer grenzschichtoptimierten Geschwindigkeitsverteilung für aerodynamisch hochbelastete Verdichtergitter
UniBw München (Fottner, Wagner, Kappler), Prüfung: 13.03.1987