Tomas Grönstedt
Tomas Grönstedt
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Evaluating the climate impact of aviation emission scenarios towards the Paris agreement including COVID-19 effects
V Grewe, A Gangoli Rao, T Grönstedt, C Xisto, F Linke, J Melkert, J Middel, ...
Nature Communications 12 (1), 3841, 2021
Assessment of future aero-engine designs with intercooled and intercooled recuperated cores
KG Kyprianidis, T Grönstedt, SOT Ogaji, P Pilidis, R Singh
Conceptual design and mission analysis for a geared turbofan and an open rotor configuration
L Larsson, T Gro¨ nstedt, KG Kyprianidis
Turbo Expo: Power for Land, Sea, and Air 54617, 359-370, 2011
Techno-economic review of alternative fuels and propulsion systems for the aviation sector
K Dahal, S Brynolf, C Xisto, J Hansson, M Grahn, T Grönstedt, M Lehtveer
Renewable and Sustainable Energy Reviews 151, 111564, 2021
Development of methods for analysis and optimization of complex jet engine systems
T Grönstedt
PQDT-Global, 2000
Optimization study of an intercooled recuperated aero-engine
L Xu, KG Kyprianidis, TUJ Grönstedt
Journal of Propulsion and Power 29 (2), 424-432, 2013
Design and analysis of an intercooled turbofan engine
L Xu, T Grönstedt
First and second law analysis of future aircraft engines
T Grönstedt, M Irannezhad, X Lei, O Thulin, A Lundbladh
Journal of Engineering for Gas Turbines and Power 136 (3), 031202, 2014
Ultra low emission technology innovations for mid-century aircraft turbine engines
T Grönstedt, C Xisto, V Sethi, A Rolt, N García Rosa, A Seitz, K Yakinthos, ...
Turbo Expo: Power for Land, Sea, and Air 49743, V003T06A001, 2016
Multidisciplinary analysis of a geared fan intercooled core aero-engine
KG Kyprianidis, AM Rolt, T Grönstedt
Journal of engineering for gas turbines and power 136 (1), 011203, 2014
The efficiency of a pulsed detonation combustor–axial turbine integration
C Xisto, O Petit, T Grönstedt, A Rolt, A Lundbladh, G Paniagua
Aerospace Science and Technology 82, 80-91, 2018
Identifiability in multi-point gas turbine parameter estimation problems
TUJ Gro¨ nstedt
Turbo Expo: Power for Land, Sea, and Air 3607, 9-17, 2002
Proof of concept study for fuselage boundary layer ingesting propulsion
A Seitz, AL Habermann, F Peter, F Troeltsch, A Castillo Pardo, ...
Aerospace 8 (1), 16, 2021
Model-based on-board turbofan thrust estimation
M Henriksson, T Grönstedt, C Breitholtz
Control Engineering Practice 19 (6), 602-610, 2011
Consistent conceptual design and performance modeling of aero engines
S Samuelsson, KG Kyprianidis, T Grönstedt
Turbo Expo: Power for Land, Sea, and Air 56673, V003T06A017, 2015
Low pressure system component advancements and its impact on future turbofan engine emissions
K Kyprianidis, D Au, SOT Ogaji, T Grönstedt
XIX International Symposium on Air Breathing Engines (ISABE), ISABE-2009-1276, 2009
Multidisciplinary design of a three stage high speed booster
M Lejon, T Grönstedt, N Glodic, P Petrie-Repar, M Genrup, A Mann
Turbo Expo: Power for Land, Sea, and Air 50794, V02BT41A037, 2017
Distributed propulsion and turbofan scale effects
A Lundbladh, T Grönstedt
ISABE 2005, 17th Symposium on Airbreathing Engine, 2005
Conceptual design of a two-pass cross-flow aeroengine intercooler
X Zhao, T Grönstedt
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2015
A comparative study of genetic algorithms and gradient methods for RM12 turbofan engine diagnostics and performance estimation
T Gro¨ nstedt, M Wallin
Turbo Expo: Power for Land, Sea, and Air 41677, 615-624, 2004
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