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Oil Film Dynamics In Aero Engine Bearing Chambers Fundamental Investigations And Numerical Modelling 1st Edition Amir A Hashmi

  • SKU: BELL-51627226
Oil Film Dynamics In Aero Engine Bearing Chambers Fundamental Investigations And Numerical Modelling 1st Edition Amir A Hashmi
$ 31.00 $ 45.00 (-31%)

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Oil Film Dynamics In Aero Engine Bearing Chambers Fundamental Investigations And Numerical Modelling 1st Edition Amir A Hashmi instant download after payment.

Publisher: Logos Verlag Berlin
File Extension: PDF
File size: 10.02 MB
Pages: 164
Author: Amir A. Hashmi
ISBN: 9783832593650, 3832593659
Language: English
Year: 2012
Edition: 1

Product desciption

Oil Film Dynamics In Aero Engine Bearing Chambers Fundamental Investigations And Numerical Modelling 1st Edition Amir A Hashmi by Amir A. Hashmi 9783832593650, 3832593659 instant download after payment.

Aero engine bearing chambers are complex machine elements inside the engines, supporting up to three concentric shafts on bearings. For safety reasons, the aero engines always employ rolling-element type bearings and therefore require a sufficient oil supply for lubrication in order to guarantee a reliable operation. As a consequence, a complex two-phase flow consisting of oil and sealing air governs the bearing chambers. A highly dynamic oil film, flowing along the chamber walls, plays a vital role to fulfill the tasks of cooling, lubricating and cleaning the bearing chambers. The design and optimization process of the bearing chambers requires a detailed understanding in order to accurately simulate the film behaviour inside the bearing chambers. Based on the earlier experimental investigations, it is known that near the scavenge off-take a relatively thick film exists. The numerical model to simulate these films must therefore take into account the elliptical behaviour of such films. Among the different models, the Volume Of Fluid (VOF) Model offers the best compromise between accuracy and efforts. However, preliminary attempts to model a fully developed and turbulent test case from literature revealed an unphysical pressure drop and velocity profile in the gas phase above the film flow. An inadequate turbulence modelling near the gas-liquid interface was identified as the problem source. The 2-Equation turbulence models (k-epsilon;ε & k-#65533;%ω) were extended to achieve a substantial improvement.

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