Isak Jonsson
Isak Jonsson arbetar sedan juli 2015 med experimentell fluiddynamik i vindtunnellaboratoriet för strömningslära. Som forskningsingenjör arbetar han främst med är att konstruera och utveckla experimentella riggar och metoder för både interna och externa intressenter. Målsättningen är att effektivt leverera högkvalitativ data och utveckla metoder för att åstadkomma detta.
Visar 36 publikationer
EXPERIMENTAL AND NUMERICAL STUDY ON THE EFFECT OF OGV CLOCKING ON ICD PERFORMANCE
Moving towards TRL 3 Intercooling Integration for Hydrogen Fueled Aircraft
Compact Heat Exchangers with Curved Fins for Hydrogen Turbofan Intercooling
The heat transfer potential of compressor vanes on a hydrogen fueled turbofan engine
Numerical study of a generic ship’s airwake for understanding bi-stability mechanism
Compact heat exchangers for hydrogen-fueled aero engine intercooling and recuperation
LOW-SPEED PROPELLER FOR UAV APPLICATIONS, FROM DESIGN TO EXPERIMENTAL EVALUATION
LESSONS LEARNED FROM PROJECT BASED TEACHING IN AEROSPACE AT CHALMERS
Compact Heat Exchangers With Curved Fins for Hydrogen Turbofan Intercooling
Lessons Learned from Project Based Teaching in Aerospace at Chalmer
Numerical modeling of laminar-turbulent transition in an interconnecting compressor duct
Multidisciplinary assessment of a year 2035 turbofan propulsion system
Effect of heat exchanger integration in aerodynamic optimization of an aggressive S-duct
EFFECT OF HEAT EXCHANGER INTEGRATION IN AERODYNAMIC OPTIMISATION OF AN AGGRESSIVE S-DUCT
Experimental Aerothermal Study of Internal Jet Engine Structures
Conceptual Design of a Compressor Vane- HEX for LH2 Aircraft Engine Applications
Experimental Aerothermal Study on Internal Jet Engine Structures
Experimental Study of Transition in a Turbine Rear Structure
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
Infrared thermography investigation of heat transfer on outlet guide vanes in an engine exit module
EFFECT OF SURFACE ROUGHNESS ON AERODYNAMIC PERFORMANCE OF TURBINE REAR STRUCTURE
Experimental aero- and thermal investigation for a next generation engine exit module.
Surface roughness impact on secondary flow and losses in a turbine exhaust casing
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Visar 4 forskningsprojekt
SWITCH - Sustainable Water-Injecting Turbofan Comprising Hybrid-electrics
Experimentell aerotermisk studie av nästa generations flygmotorkomponenter
Enabling cryogenic hydrogen-based CO2-free air transport (ENABLEH2)
Aerodynamik för Robusta och Optimerade Strukturer