Publications - GasTurb

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The book Gasturbinen - Betriebsverhalten und Optimierung was published 1975, during my time at the Flight Propulsion Institute (Professor H.G. Muenzberg) of the Technical University of Munich. Many of the formulae and algorithms used within GasTurb can be found in that book, which is unfortunately no longer available.

As a member of several working groups I have contributed to the following reports:

Propulsion and Energetics Panel Working Group 24:
Recommended Practices for the Assessment of the Effects of Atmospheric Water Ingestion on the Performance and Operability of Gas Turbine Engines
AGARD Advisary Report No. 332, 1995

RTO Applied Vehicle Technology Panel (AVT) Task Group AVT-018:
Performance Prediction and Simulation of Gas Turbine Engine Operation
RTO Technical Report 044, 2002

SAE Committee E-33 Inflight Propulsion Measurement Committee
In-Flight Thrust Determination
Draft  SAE AIR 1703, 2006

During the 1995 ASME conference in Houston,TX, USA the first paper about GasTurb was published. This was followed by a long row of presentations at the yearly Turbo Expo of the International Gas Turbine Institute IGTI.

Where
When

Title

Tool Used

AGARD
1992

Calculation of Installation EffectsWithin PerformanceComputer Programs
Joachim Kurzke
in: Steady and Transient Performance Prediction of Gas Turbine Engines
AGARD Lecture Series 183

Houston
USA, 1995

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

GasTurb 6

Birmingham
UK, 1996

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

Smooth C
Smooth T

Orlando
USA, 1997

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

GasTurb 7

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

GasTurb 7

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

Smooth C

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

RTO
2002

Performance Prediction and Simulation of

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

GasTurb 9
GasTurb Details 4

Atlanta
USA, 2003

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

GasTurb 10

Rhode-Saint-Genèse Belgium
2003

Preliminary Design
Joachim Kurzke
in: Aero-Engine Design: A State of the Art, VKI Lecture Series 2003-06

GasTurb 10

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

GasTurb 10

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

GasTurb 10

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)

GasTurb 10

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

GasTurb 11

Montreal
Canada
2007

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

GasTurb 11

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

GasTurb 11

Rhode-Saint-Genèse Belgium2008

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

GasTurb 11

Orlando
USA
2009

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

GasTurb 11

Rhode-Saint-Genèse Belgium
and
Dayton, USA
2010

The Mission Defines the Cycle: Turbojet, Turbofan and Variable Cycle Engines for High Speed Propulsion
VKI Lecture Series 2010 High Speed Propulsion: Engine Design, Integration and Thermal Management
RTO-EN-AVT-185

GasTurb 11

Vancouver
Canada
2011

Correlations Hidden in Compressor Maps
Joachim Kurzke
ASME GT2011-45519

Smooth C

Gothenburg
Sweden
2011

Transient Simulations During Preliminary Conceptual Engine Design
Joachim Kurzke
ISABE 2011-1321

GasTurb 12

Rhode-Saint-Genèse Belgium2013

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

GasTurb 12

Busan
Korea 2013

Modeling the Thrust Management of Commercial Airliners
Joachim Kurzke
ISABE 2013-1430

GasTurb 12

 
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