Blade tip clearances in gas turbine engines are strongly affected by heat transfer on rotating
disc surfaces as it determines the temperature and in turn the radial growth of rotating discs …

The prediction of compressor drum cavity heat transfer is an important factor in the overall
design of an aero engine. The rotationally dominated flow field within the cavity governs the …

Conduction in thin disks can be modeled using the fin equation, and there are analytical
solutions of this equation for a circular disk with a constant heat-transfer coefficient …

This paper describes the modeling of typical secondary air system elements such as rotating
orifices, seals, and flow passages with heat and work transfer from the surrounding surfaces …

Experimental measurements of heat transfer are made from the inner peripheral surface of a
rotating test rig designed to be similar to a gas turbine high pressure compressor internal air …

Abstract Development of passive cooling systems for electronic devices demands the
multiparametric analysis of main heat transfer mechanisms inside the domains with heat …

This study experimentally and numerically analyzes the effect of the coolant cross-flow on
film-cooling effectiveness. The three kinds of film holes considered are cylindrical, fan …

The buoyancy-affected flow in rotating disk cavities, such as occurs in compressor disk
stacks, is known to be complex and difficult to predict. In the present work, large eddy …

We introduce a deep learning accelerated methodology to solve PDE-based Bayesian
inverse problems with guaranteed accuracy. This is motivated by solving the ill-posed …

Flow and heat transfer in an aero-engine compressor disk cavity with radial inflow has been
studied using computational fluid dynamics (CFD), large eddy simulation (LES), and …