[1] Grönstedt T., Johansson T. and Håll U., “The Optimization of a Seven Stage Compressor”,
International Symposium on Fluid Machinery and Fluid Engineering,
Sept. 9-12, 1996, Beijing, China

[2] Grönstedt T. and Håll U., “Mission Dependent Optimization of Advanced Fighter Engines”,
13th International Symposium on Air Breathing Engines,
Sept. 7-12, 1997, Chattanooga, Tennessee, U.S.A.

[3] Grönstedt T., “Advanced Solvers for General High Performance Transient Gas Turbine Simulation Tools”,
14th International Symposium on Air Breathing Engines,
Sept. 5-12, 1999, Florence, Italy.

[4] Grönstedt T. and Pilidis P., “Control Optimization of the Transient Performance of the
Selective Bleed Variable Cycle Engine During Mode Transition
”,
ASME Turbo Expo: Land, Sea & Air 8-11 May 2000,
Munich.

--------------- Post Ph. D. publications

[5] Grönstedt T., “A Multi-point Gas Path Analysis Tool for Gas Turbine Engines with a
Moderate Level of Instrumentation
”, 15th International Symposium on Air Breathing Engines,
Sept. 3-7, 2001, Bangalore, India.

[6] Sjöberg, J., Fyhr, F. and Grönstedt, T., “Estimating Parameters in Physical Models using
MathModelica
”, Proceedings of the 2ndInternational Modelica Conference, Deutsche
Zentrum für Luft- und Raumfahrt e.V., Oberpfaffenhofen, Germany, pp. 325-330, 2002.

[7] Grönstedt T. and Pilidis P., “Control Optimization of the Transient Performance
of the Selective Bleed Variable Cycle Engine During Mode Transition
”, Journal of
Engineering for Gas Turbines and Power.
Jan. 2002, pp. 75-81.

[8] Grönstedt T. “Identifiability in multi-point gas turbine parameter estimation problems”,
Proceedings of Turbo Expo 2002, ASME Turbo Expo: Land, Sea & Air 3-6 June 2002,
Amsterdam.

[9] Wallin, M., Grönstedt, T., and Håll, U., ”A Mission Based Optimisation Study of Engine
Configurations For a Low-Signature Reconnaissance UAV- A Multi-Objective Approach
”,
AIAA-2003-6528, 2nd AIAA “Unmanned Unlimited” Systems, Technologies, and Operations,
 
San Diego, 2003.

[10] Wallin, M., Grönstedt, T., and Håll, U., ”A Study of Engine Configurations for a Low-Signature
Reconnaissance UAV
”, ISABE-2003-1093, XVI International Symposium on Air Breathing Engines,
Cleveland, Ohio, 2003.

[11] Wallin, M., Håll, U., and Grönstedt, T., ”Effects of Engine Intake and Nozzle Design the
Performance of a Low-Signature Reconnaissance UA,
, 40th AIAA/ASME/SAE/ASEE Joint
Propulsion Conference and Exhibit
,
Fort Lauderdale, Florida, 2004.

[12] Skölde, P., Wallin M. and Grönstedt, T., ”An Augmented Multi-Point Estimation
Technique for Gas Path Analysis Model Generation
”, Proceedings of Turbo Expo 2004,
ASME Turbo Expo: Land, Sea & Air 14-17 June 2004,
Vienna.

[13] Grönstedt, T. and Wallin, M., “A Comparative Study of Genetical Algorithms and Gradient Methods
for RM12 Engine Diagnostics and Performance Estimation
”, ASME Turbo Expo, Vienna 2004.

[14] Henriksson M. and Grönstedt T., “Engine Variability Impact on Reduced Order
Thrust Estimation Filters
”, 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
and Exhibit,
Fort Lauderdale, Florida 11 - 14 Jul 2004.

[15] Grönstedt T. and Zhao Y., “A Numerically Efficient Method for Transient Gas
Turbine Performance Estimation
”, 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
and Exhibit,
Fort Lauderdale, Florida 11 - 14 Jul 2004.