Myles Zabel, M.Sc.

Institute of Aerospace Thermodynamics, ITLR, University of Stuttgart

As part of his research activities in sub-project A02, Myles Zabel is investigating how flow losses in aircraft flows can be determined using the second law of thermodynamics. Particularly in combination with heat transfer, various effects are superimposed in integrated propulsion systems, which complicates the conventional determination of flow losses.

He also examines the intensification of heat transfer through microstructures.

ORCiD: 

0009-0008-6370-6867

Institute: 

Myles Zabel´s Research facility