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Publikationen am Fachgebiet Luftfahrtantriebe

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2013

Impact of Hub Clearance on Endwall Flow in a Highly Loaded Axial Compressor Stator [13]

Beselt, C. and van Rennings, R. and Peitsch, D. and Thiele, F.

ASME Turbo Expo 2013: Turbine Technical Conference and Exposition, GT2013-95463. 2013

Link zur Publikation [14] Download Bibtex Eintrag [15]

Experimental Investigations of Endwall Flow in a Highly Loaded Annular Compressor Stator Cascade [16]

Beselt, C. and Peitsch, D.

ETC - 10th European Conference on Turbomachinery Fluid dynamics & Thermodynamics, ETC2013-152. 2013

Link zur Publikation [17] Download Bibtex Eintrag [18]

Influence of the Clearance Size on Rotating Instability in an Axial Compressor Stator [19]

Beselt, C. and Pardowitz, B. and van Rennings, R. and Sorge, R. and Peitsch, D. and Enghardt, L. and Thiele, F. and Ehrenfried, K. and Thamsen, P. U.

ETC - 10th European Conference on Turbomachinery Fluid dynamics & Thermodynamics, ETC2013-141. 2013

Link zur Publikation [20] Download Bibtex Eintrag [21]

2012

Transition Mechanisms in Laminar Separated Flow Under Simulated Low Pressure Turbine Aerofoil Conditions [22]

Dähnert, J. and Lyko, C. and Peitsch, D.

Journal of Turbomachinery. ASME, TURBO-11-1120. 2012

Link zur Publikation [23] Download Bibtex Eintrag [24]

Powering the World – High Technology in Gas Turbines [25]

Peitsch, Dieter

Rozwój Techniki, Technologii i Transportu w Lotnictwie 2012

Download Bibtex Eintrag [26]

Some Aspects on Wet Compression - Physical Effects and Modeling Strategies used in Engine Performance Tools [27]

Obermüller, M. and Schmidt, K.-J. and Schulte, H. and Peitsch, D.

Deutscher Luft- und Raumfahrtkongress, 281210. 2012

Link zur Publikation [28] Download Bibtex Eintrag [29]

Identifikation einer Regelgröße zur aktiven Strömungskontrolle an einer linearen Verdichterkaskade im kompressiblen Machzahlbereich [30]

Tiedemann, C. and Steinberg, S. and Peitsch, D. and King, R.

Deutscher Luft- und Raumfahrtkongress, 281267. 2012

Link zur Publikation [31] Download Bibtex Eintrag [32]

Experimental and Numerical Investigations of Rotating Instability Phenomenon in An Axial Compressor Stator [33]

Beselt, C. and Peitsch, D. and van Rennings, R. and Thiele, F.

AIAA - 42nd Fluid Dynamics Conference and Exhibit. American Institute of Aeronautics and Astronautics. 2012

Link zur Publikation [34] Download Bibtex Eintrag [35]

A New Linear High Speed Compressor Stator Cascade for Active Flow Control Investigations [36]

Tiedemann, C. and Heinrich, A. and Peitsch, D.

AIAA - 6th Flow Control Conference. American Institute of Aeronautics and Astronautics. 2012

Link zur Publikation [37] Download Bibtex Eintrag [38]

On the Effect of Volute Tongue Design on Radial Turbine Performance [39]

Suhrmann, J. and Peitsch, D. and Gugau, M. and Heuer, T.

ASME Turbo Expo 2012: Turbine Technical Conference and Exposition, pp. 891-901, GT2012-69525. 2012

Link zur Publikation [40] Download Bibtex Eintrag [41]

Influence of Mach Number and Aerodynamic Loading on Rotating Instability in an Annular Compressor Cascade [42]

Beselt, C. and Peitsch, D.

ASME Turbo Expo 2012: Turbine Technical Conference and Exposition, pp. 2711-2720, GT2012-69393. 2012

Link zur Publikation [43] Download Bibtex Eintrag [44]

2011

Validation and Development of Models for Optimum Wheel Flow Outlet Angles of Small Size Radial Turbines [45]

Suhrmann, J. and Peitsch, D. and Gugau, M. and Heuer, T.

IGTC - International Gas Turbine Congress, IGTC2011-162-2. 2011

Download Bibtex Eintrag [46]

Validation and Development of Models for Optimum Wheel Flow Inlet Angles of Small Size Radial Turbines [47]

Suhrmann, J. and Peitsch, D. and Gugau, M. and Heuer, T.

IGTC - International Gas Turbine Congress, IGTC2011-162-1. 2011

Download Bibtex Eintrag [48]

Transition Mechanisms in Laminar Separated Flow under Unsteady Main Flow Conditions - Part II: Unsteady Flowfield [49]

Lyko, C. and Dähnert, J. and Peitsch, D.

IGTC - International Gas Turbine Congress, IGTC2011-0255. 2011

Download Bibtex Eintrag [50]

Transition Mechanisms in Laminar Separated Flow under Unsteady Main Flow Conditions - Part I: Steady Flowfield [51]

Lyko, C. and Dähnert, J. and Peitsch, D.

IGTC - International Gas Turbine Congress, IGTC2011-0254. 2011

Download Bibtex Eintrag [52]

Challenges for the Development of Advanced Propulsion Systems for Aircraft [53]

Peitsch, Dieter

International Congress on Thermodynamics 2011

Download Bibtex Eintrag [54]

Strömungsinduzierter Schall in Turbomaschinen – Die Rotierende Instabilität [55]

Beselt, C. and Peitsch, D. and Pardowitz, B. and Enghardt, L.

Deutscher Luft- und Raumfahrtkongress, 241377. 2011

Link zur Publikation [56] Download Bibtex Eintrag [57]

Hot-Acoustic-Testrig (HAT): A Unique Facility for Thermoacoustic Research [58]

Knobloch, K. and Lahiri, C. and Enghardt, L. and Bake, F. and Peitsch, D.

ASME Turbo Expo 2011: Turbine Technical Conference and Exposition, pp. 1023-1032, GT2011-45705. 2011

Link zur Publikation [59] Download Bibtex Eintrag [60]

Transition Mechanisms in Laminar Separated Flow Under Simulated Low Pressure Turbine Airfoil Conditions [61]

Dähnert, J. and Lyko, C. and Peitsch, D.

ASME Turbo Expo 2011: Turbine Technical Conference and Exposition, pp. 1575-1587, GT2011-45690. 2011

Link zur Publikation [62] Download Bibtex Eintrag [63]

Propelling the Future - The Meaning of ACARE VISION 2050 for the Future Development of Propulsion Systems for Aircraft [64]

Peitsch, Dieter

PTNSS - 4th International Congress on Combustion Engines, PTNSS-2011-SS4-401. 2011

Download Bibtex Eintrag [65]

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