Leonhard Fottner

发表

Experiments in Active Stall Control of a Twin-Spool Turbofan Engine

Armin Orthmann, Dirk C. Leinhos, Stephen G. Scheidler, 2002 .

The Use of Hot-Wire Anemometry to Investigate Unsteady Wake-Induced Boundary-Layer Development on a High-Lift LP Turbine Cascade

Stefan Brunner, Leonhard Fottner, Stefan Wolff, 2000 .

The Influence of Technical Surface Roughness of Modern Blade Manufacturing Methods on the Flow Around a Compressor Cascade

Leonhard Fottner, Robert Leipold, Matthias Boese, 1999 .

The Influence of Load Distribution on Secondary Flow in Straight Turbine Cascades

Leonhard Fottner, Andreas P. Weiß, 1993 .

EXPERIMENTAL INVESTIGATION OF BOUNDARY LAYER TRANSITION AND TURBULENCE STRUCTURES ON A HIGHLY LOADED COMPRESSOR CASCADE

Leonhard Fottner, Dirk Wunderwald, L. Fottner, 1995 .

Experimental Operating Range Extension of a Twin-Spool Turbofan Engine by Active Stability Control Measures

Leonhard Fottner, Stephan G. Scheidler, 2004 .

Investigations of Shock/Boundary-Layer Interaction in a Highly Loaded Compressor Cascade

Leonhard Fottner, Ralf M. Bell, L. Fottner, 1995 .

A Presentation of Detailed Experimental Data of a Suction Side Film Cooled Turbine Cascade

Holger Brandt, Leonhard Fottner, Wolfgang Ganzert, 2000 .

Comparison of Two Highly Loaded Low Pressure Turbine Cascades Under the Influence of Wake-Induced Transition

Stefan Brunner, Heinz-Peter Schiffer, Leonhard Fottner, 2000 .

Experimental Investigation of Turbulence Structures in the Boundary Layer of a Highly Loaded Turbine Cascade

Leonhard Fottner, Dirk Wunderwald, 1996 .

Steady Performance Measurements of a Turbofan Engine With Inlet Distortions Containing Co- and Counterrotating Swirl From an Intake Diffuser for Hypersonic Flight

Dirk C. Leinhos, Leonhard Fottner, Norbert R. Schmid, 2001 .

Stall Inception in the Compressor System of a Turbofan Engine

Leonhard Fottner, Bernd Höss, Dirk C. Leinhos, 1998 .

Experimental Investigation of Heat Transfer in Separated Flow on a Highly Loaded LP Turbine Cascade

Leonhard Fottner, Stefan Wolff, Lars Homeier, 2003 .

STALL INCEPTION IN A 5-STAGE HP-COMPRESSOR WITH INCREASED LOAD DUE TO INLET DISTORTION

Leonhard Fottner, Thomas Peters, Werner Jahnen, 1999 .

Numerical Investigation of the Wake-Boundary Layer Interaction on a Highly Loaded LP Turbine Cascade Blade

Leonhard Fottner, Pasquale Cardamone, Peter Stadtmu¨ller, 2002 .

Highly Loaded Tandem Compressor Cascade With Variable Camber and Stagger

Leonhard Fottner, Johann Sachmann, 1993 .

Experimental operating range extension of a twin-spool turbofan engine by active stability control measures

Leonhard Fottner, Stephan G. Scheidler, 2006 .

A Test Case for the Numerical Investigation of Wake Passing Effects on a Highly Loaded LP Turbine Cascade Blade

Leonhard Fottner, Peter Stadtmüller, L. Fottner, 2001 .

The Influence of Inlet Swirl Distortions on the Performance of a Jet Propulsion Two-Stage Axial Compressor

Leonhard Fottner, Wolfram Pazur, 1990 .

Overview on Test Cases for Computation of Internal Flows in Turbomachines

Leonhard Fottner, 1989 .

Closure to “Discussion of ‘The Influence of Technical Surface Roughness Caused by Precision Forging on the Flow Around a Highly Loaded Compressor Cascade’ ” [ASME J. Turbomach., 122, No. 3, p. 424 (2000)]

Leonhard Fottner, Matthias Boese, Robert Leipold, 2000 .

The Influence of Inlet Swirl Distortions on the Performance of a Jet Propulsion Two-Stage Axial Compressor

Leonhard Fottner, Wolfram Pazur, L. Fottner, 1990 .

Effects of Co- and Counter-Rotating Inlet Distortions on a 5-Stage HP-Compressor

Leonhard Fottner, Thomas Peters, 2002 .

Effects of Rotating Inlet Distortion on a 5-Stage HP-Compressor

Leonhard Fottner, Thomas Peters, Thomas Bürgener, 2001 .

Performance Improvements of Compressor Cascades by Controlling the Profile and Sidewall Boundary Layers

Leonhard Fottner, Wolfgang Sturm, Hermann Scheugenpflug, 1991 .

Stall inception in the compressor system of a turbofan engine

Dirk C. Leinhos, Leonhard Fottner, Bernd Höss, 2000 .

A Numerical Study of the Influence of Grid Refinement and Turbulence Modelling on the Flow Field Inside a Highly Loaded Turbine Cascade

Leonhard Fottner, Thomas Hildebrandt, L. Fottner, 1998 .

The Influence of Technical Surface Roughness Caused by Precision Forging on the Flow Around a Highly Loaded Compressor Cascade

Leonhard Fottner, Matthias Boese, M. Boese, 2000 .

Experimental and Numerical Investigation of Flapping Wing Propulsion and its Application for Boundary Layer Control

Max F. Platzer, Leonhard Fottner, C. M. Dohring, 1998 .

The Influence of Transient Inlet Distortions on the Instability Inception of a Low Pressure Compressor in a Turbofan Engine

Dirk C. Leinhos, Leonhard Fottner, Norbert R. Schmid, 2000 .

Controlling the secondary flow in a turbine cascade by three-dimensional airfoil design and endwall contouring

I. Raab, Leonhard Fottner, Arno Duden, 1999 .

Three-Dimensional Flow Analysis of Turbine Blade Cascades with Leading-Edge Ejection

Dieter Bohn, Karsten Kusterer, Leonhard Fottner, 2000 .

Experimental and Numerical Investigation of Wake-Induced Transition on a Highly Loaded LP Turbine at Low Reynolds Numbers

Leonhard Fottner, Andreas Fiala, Peter Stadtmüller, 2000 .

Flow Field Measurements on a Large Scale Turbine Cascade With Leading Edge Film Cooling by Two Rows of Holes

Leonhard Fottner, Sabine Ardey, L. Fottner, 1997 .

Calculations of Effects of Rotating Inlet Distortion on Flow Instabilities in Compression Systems

Leonhard Fottner, Jun Hu, 1995 .

Investigation of the Boundary Layer Development on a Highly Loaded Low Pressure Turbine Cascade Under the Influence of Unsteady Flow Conditions

Leonhard Fottner, Paola Acton, 1998 .

Surface Roughness Effects on Turbine Blade Aerodynamics

Leonhard Fottner, Frank Hummel, Michael Lötzerich, 2005 .

A Systematic Experimental Study on the Aerodynamics of Leading Edge Film Cooling on a Large Scale High Pressure Turbine Cascade

Leonhard Fottner, Sabine Ardey, 1998 .

Turbulence Structures of Leading Edge Film Cooling Jets

Leonhard Fottner, Sabine Ardey, Stefan Wolff, 2000 .

The Influence of Transient Inlet Distortions on the Instability Inception of a Low Pressure Compressor in a Turbofan Engine

Dirk C. Leinhos, Leonhard Fottner, Norbert R. Schmid, 2001 .

The Aerodynamic Mixing Effect of Discrete Cooling Jets With Mainstream Flow on a Highly Loaded Turbine Blade

Leonhard Fottner, Günter Wilfert, 1994 .

Effects of Riblets on the Loss Behavior of a Highly Loaded Compressor Cascade

Leonhard Fottner, Matthias Boese, 2002 .

The Aerodynamic Mixing Effect of Discrete Cooling Jets With Mainstream Flow on a Highly Loaded Turbine Blade

Leonhard Fottner, L. Fottner, Günter Wilfert, 1994 .

The Influence of Multimode Transition Initiated by Periodic Wakes on the Profile Loss of a Linear Compressor Cascade

Marius Swoboda, Leonhard Fottner, Stefan Brunner, 2000 .