Houston
USA, 1995

Advanced User-Friendly Gas Turbine Performance Calculations on a Personal Computer
Joachim Kurzke, ASME 95-GT-147

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Birmingham
UK, 1996

How to Get Component Maps for Aircraft Gas Turbine Performance Calculations,
Joachim Kurzke, ASME 96-GT-164

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Smooth T

Orlando
USA, 1997

Some Applications of the Monte Carlo Method to Gas Turbine Performance Simulations
Joachim Kurzke, ASME 97-GT-48

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Stockholm
Sweden,
1998

Gas Turbine Cycle Design Methodology: A Comparison of Parameter Variation with Numerical Optimization
Joachim Kurzke, ASME 98-GT-343
Journal of Engineering for Gas Turbines and Power January 1999

Toulouse
France, 1999

A mixed flow turbofan afterburner simulation for the definition of reheat fuel control laws.
Joachim Kurzke, Claus Riegler
NATO Research and Technology Organisation RTO-MP-8, AC/323(AVT)TP9

Munich,
Germany,
2000

A New Compressor Map Scaling Procedure for Preliminary Conceptional Design of Gas Turbines€�
Joachim Kurzke and Claus Riegler, ASME 2000-GT-0006
Aircraft Engine Committee Best Paper Award

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Some Aspects of Modelling Compressor Behavior in Gas Turbine Performance Calculations
Claus Riegler, Michael Bauer, Joachim Kurzke
ASME 2000-GT-0574, Journal of Turbomachinery, April 2001.

Smooth C

Amsterdam
The Netherlands
2002

Preliminary Gas Turbine Design Using the Multidisziplinary Design System Mopeds
Peter Jeschke, Joachim Kurzke, ASME GT-2002-30496
Journal of Engineering for Gas Turbines and Power April 2004

Performance Modeling Methodology: Efficiency Definitions for Cooled Single and Multistage Turbines
Joachim Kurzke, ASME GT-2002-30497

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Atlanta
USA, 2003

Model Based Gas Turbine Parameter Correction
Joachim Kurzke, ASME GT-2003-38234

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Roma
Italy, 2003

Achieving maximum thermal efficiency with the simple gas turbine cycle, Joachim Kurzke
9th CEAS European Propulsion Forum: “Virtual Engine - A Challenge for Integrated Computer Modelling”, 15-17 October 2003, Roma, Italy

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Reno,
USA, 2005

How to Create a Performance Model of a Gas Turbine From a Limited Amount of Information
Joachim Kurzke, ASME GT 2005-68537

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Munich
Germany
2005

Sensor Checking Using Model Based Engine Performance Test Analysis and Numerical Optimization, Joachim Kurzke, 17th International Symposium on Airbreathing Engines (ISABE), Munich (September 2005)

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Barcelona
Spain, 2006

Effects of Inlet Flow Distortion on the Performance of Aircraft Gas Turbines,
Joachim Kurzke ASME GT2006-90419
Journal of Engineering for Gas Turbines and Power in April 2008

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Montreal
Canada
2007

About Simplifications in Gas Turbine Performance Calculations
Joachim Kurzke, ASME GT2007-27620

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Honolulu
Hawaii
2008

The Importance of Component Maps for Gas Turbine Performance Simulations
Joachim Kurzke, 12th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, Feb 17-22, 2008

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Rhode-Saint-Genèse Belgium, 2008

Preliminary Design
Aeroengine Design: From State of the Art Turbofans Towards Innovative Architectures, VKI Lecture Series 2008-04, 3-7 March 2008

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Orlando
USA
2009

Fundamental differences between conventional and geared turbofans
Joachim Kurzke, ASME GT2009-59745

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