Isak Jonsson
Isak Jonsson has been working since July 2015 with experimental fluid dynamic in the wind tunnel laboratory at the department of fluid dynamics. As a researcher he works with designing and constructing experimental facilities and methods for both internal and external clients. Isak is also operational manager of Chalmers laboratory of fluids and thermal sciences, a chalmers infrastructure.
Showing 36 publications
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
LESSONS LEARNED FROM PROJECT BASED TEACHING IN AEROSPACE AT CHALMERS
Compact heat exchangers for hydrogen-fueled aero engine intercooling and recuperation
LOW-SPEED PROPELLER FOR UAV APPLICATIONS, FROM DESIGN TO EXPERIMENTAL EVALUATION
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
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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Showing 5 research projects
Ultra Short Engine low-pressure turbine Interactions with Turbine rear structure
SWITCH - Sustainable Water-Injecting Turbofan Comprising Hybrid-electrics
Experimental Aero- and Thermal investigation for a next generation Engine Exit Module (EATEEM)
Enabling cryogenic hydrogen-based CO2-free air transport (ENABLEH2)
Aerodynamics in Robust and Optimized Structures