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Document type:
Master's thesis
Author(s):
Khot, Ankit
Title:
Computational Simulation of Heat Transfer Effect on Aerodynamic Performance of an Aircraft Wing
Abstract:
The electrification of propulsion systems in hybrid and electric aircraft increases its cooling demands. The conventional heat exchangers contribute to the overall drag of an aircraft, and alternate cooling techniques are necessary. An earlier study done at Bauhaus- Luftfahrt e.V. explores the potential of using aircraft surface for cooling purposes using semi-empirical relations, and the current work is the outlook of this exploratory study. Heat transfer from the aircraft surfaces can alter it...     »
Keywords:
heat transfer, heated airfoil, hybrid and electric aircraft, SU2, RANS, compressible flows
Subject:
Hydromechanics
Year:
2021
Month:
May
Language:
en
University:
Technische Universität München
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