Thermal Performance Evaluation in Gas Turbine Aero Engines Accessory Gearbox

This paper presents a methodological approach for mathematical modelling and physics-based analysis of accessory gearbox (AGB) thermal behavior in gas turbine aero engines. The AGB structure, as one of the main sources of heat in gas turbine aero engines, is firstly described and its power losses wi...

Full description

Bibliographic Details

Published in:	International Journal of Turbomachinery, Propulsion and Power
Main Authors:	Soheil Jafari, Ahmed Bouchareb, Theoklis Nikolaidis
Format:	Article
Language:	English
Published:	MDPI AG 2020-08-01
Subjects:	thermal management systems accessory gearbox gas turbine aero engines heat loss mechanisms thermal performance evaluation
Online Access:	https://www.mdpi.com/2504-186X/5/3/21