Tomas Grönstedt
Mer information om Tomas Grönstedt finns på Chalmers engelska sidor.
Visar 106 publikationer
Quantifying the Environmental Design Trades for a State-of-the-Art Turbofan Engine
Development of fuel and heat management systems for liquid hydrogen powered aircraft
Feasibility Study of a Radical Vane-Integrated Heat Exchanger for Turbofan Engine Applications
Conceptual Design of a Compressor Vane- HEX for LH2 Aircraft Engine Applications
Wake Analysis of an Aerodynamically Optimized Boxprop High Speed Propeller
Assessment of CO2 and NOx emissions in intercooled pulsed detonation turbofan engines
Concetual design of ultra-efficient cores for mid-century aircraft turbine engines
Flygforskare: "Våra beräkningar bygger på detaljerade modeller"
Numerical investigation of film and impingement cooling schemes for gas turbine application
Wake Energy Analysis Method Applied to the Boxprop Propeller Concept
The Efficiency of a Pulsed Detonation Combustor-Axial Turbine Integration
Propulsive efficiency of boundary layer ingestion propellers
First and Second Law Analysis of Radical Intercooling Concepts
DN Debatt. "Mellanlandning kan halvera utsläppen från Thailandsresa"
Assessment of CO2 and NOx emissions in intercooled pulsed detonation turbofan engines
Aerodynamic and aeroacoustic comparison of optimized high-speed propeller blades
Scale effects on conventional and intercooled turbofan engine performance
Numerical Simulation of Nacelle Flowfield for Counter-Rotating Open Rotor Propellers
Experimental Validation of the Aerodynamic Characteristics of an Aero-engine Intercooler
Multidisciplinary Design of a Three Stage High Speed Booster
On Improving the Surge Margin of a Tip-Critical Axial Compressor Rotor
First and second law analysis of radical intercooling concepts
Analytical model for the performance estimation of pre-cooled pulse detonation turbofan engines
Optimization of Robust Transonic Compressor Blades
First and second law analysis of intercooled turbofan engine
An Optimization Platform for High Speed Propellers
Wake and Loss Analysis for a Double Bladed Swept Propeller
A Search for the “ULTIMATE” Aero-Engine
A Noise Assessment framework for Subsonic Aircraft and Engines
An outlook for radical aero engine intercooler concepts
ULTRA LOW EMISSION TECHNOLOGY INNOVATIONS FOR MID-CENTURY AIRCRAFT TURBINE ENGINES (presentation)
Ultra low emission technology innovations for mid-century aircraft turbine engines
First and second law analysis of intercooled turbofan engine
High Power Density Work Extraction from Turbofan Exhaust Heat
A Mission Assessment of Aero Engine Losses
Conceptual design of a two-pass cross-flow aeroengine intercooler
Consistent Conceptual Design and Performance Modeling of Aero Engines
Aero Engine Intercooling Optimization Using a Variable Flow Path
Preparing for Proof-of-concept of a Novel Propeller for Open Rotor Engines
Exploring Influence of Static Engine Component Design Variables on System Level Performance
A Thermodynamic Analysis of Two Competing Mid-Sized Oxy-Fuel Combustion Combined Cycles
A Conceptual Design Study of an Open Rotor Powered Regional Aircraft
Multidisciplinary Analysis of a Geared Fan Intercooled Core Aero-Engine
First and Second Law Analysis of Future Aircraft Engines
The Effect of Engine Dimensions on Supersonic Aircraft Performance
Multidisciplinary Analysis of a Geared Fan Intercooled Core Aero-Engine
First and Second Law Analysis of Future Aircraft Engines
An assessment of cooled air cooling for combined cycle gas turbines
Integration of Fluid Thermodynamic and Transport Properties in Conceptual Turbomachinery Design
EFFECTS OF DIFFERENT PROPELLER MODELS ON OPEN ROTOR FUEL CONSUMPTION
Lessons Learned From the Development of Courses on Gas Turbine Multidisciplinary Conceptual Design
Transforming Propulsion Installation for Commercial Aircraft
Optimization Study of an Intercooled Recuperated Aero-Engine
Lessons learned from the development of courses on gas turbine multi-disciplinary conceptual design
A Comparative Analysis of Two Competing Mid-size Oxy-fuel Combustion Cycles
Conceptual Design Of A Mid-Sized Semi-Closed Oxy-Fuel Combustion Combined Cycle
Multicriteria Optimization Of Conceptual Compressor Aerodynamic Design
LIMITATIONS ON TUBE FILLING IN A PULSED DETONATION ENGINE
Mission optimization of the geared turbofan engine
Assessment of Future Aero-engine Designs with Intercooled and Intercooled Recuperated Cores
Conceptual Design and Mission Analysis for a Geared Turbofan and an Open Rotor Configuration
Analysis of an Intercooled Recuperated Aero-engine
Model-based on-board turbofan thrust estimation
Optimization Study of an Intercooled Recuperated Aero-Engine
Optimizing the Operation of the Intercooled Turbofan Engine
Design and Analysis of an Intercooled Turbofan Engine
Assessment of Future Aero Engine Designs with Intercooled and Intercooled Recuperated Cores
EFFECTS OF A CONTROLLED PHASE-SHIFT ON THE OUTLET CONDITIONS OF A SET OF PULSE DETONATORS
Development, accomplishment and evaluation of a project course in applied mechanics---Lessons learnt
A Contra-rotating Variable Cycle Turbofan Engine
Low Pressure System Component Advancements and its Impact on Future Turbofan Engine Emissions
Derated Climb Trajectories for Subsonic Transport Aircraft
Low Pressure System Component Advancements and Its Influence on Future Turbofan Engine Emissions
Future Innovative Cores for Commercial Engines
Mission Optimization of an Intercooled Turbofan Engine
DISTRIBUTED PROPULSION AND TURBOFAN SCALE EFFECTS
Reduced order Thrust Estimation for a Jet Engine
Least Squares Based Transient Nonlinear Gas Path Analysis
A Numerically Efficient Method for Transient Gas Turbine Performance Estimation
Effects of Engine Intake and Nozzle Design the Performance of a Low-Signature Reconnaissance UAV
An Augmented Multi-Point Estimation Technique for Gas Path Analysis Model Generation
Engine Variability Impact on Reduced Order Thrust Estimation Filters
A Study of Engine Configurations for a Low-Signature Reconnaissance UAV
Identifiability in multi-point gas turbine parameter estimation problems
Estimating Parameters in Physical Models using MathModelica
Development of Methods for Analysis and Optimization of Complex Jet Engine Systems
Advanced Solvers for General High Performance Transient Gas Turbine Simulation Tools
Mission Dependent Optimization of Advanced Fighter Engines
The Optimization of a Seven Stage Compressor
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Visar 23 forskningsprojekt
IMOTHEP - Investigation and Maturation of Technologies for Hybrid Electric Propulsion
Installed adVAnced Nacelle uHbr Optimisation and Evaluation (IVANHOE)
Sustainable aviation fuels for a carbon constrained world
Reducering av oljud från propellrar för framtida eldrivna flygplan
Enabling cryogenic hydrogen-based CO2-free air transport (ENABLEH2)
Virtuell Integrerad Demonstrator för turbomaskiner (VIND)
Sekundärflödesvärmeväxlare för Förbättring av Flygmotorers Verkningsgrad
Concept validation study for fuselage wake-fillIng propulsion integration (CENTRELINE)
Simulering av atmosfär och flygtrafik för en tystare omvärld (SAFT)
Ultra Low emission Technology Innovations for Mid-century Aircraft Turbine Engines (ULTIMATE)
Engine Module Validators (ENOVAL)
TOICA - Integrerad termiskt driven konceptualisering av flygplan
Innovativ Framdrivning och Motorinstallation
Konstruktion för Prestanda - avancerad motorarkitektur och integration
Engine Breakthrough Components and Subsystems (E-BREAK)
Conceptual gas turbine modeling for oxy-fuel cycles. Turbokraft phase 2
Low Emissions Core-Engine Technologies (LEMCOTEC)