The Effect of Initial Injection Conditions on the Oil Droplet Motion in a Simplified Bearing Chamber
Author:
Affiliation:
1. University Technology Centre in Transmission Systems, School of Mechanical, Materials and Manufacturing Engineering, University of Nottingham, Nottingham NG7 2RD, United Kingdom
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Link
http://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/doi/10.1115/1.2770480/5705700/012501_1.pdf
Reference21 articles.
1. Influence of High Rotational Speeds on Heat Transfer and Oil Film Thickness in Aero Engine Bearing Chambers;Wittig;ASME J. Eng. Gas Turbines Power
2. Glahn, A., Busam, S., and Wittig, S., 1997, “Local and Mean Heat Transfer Coefficients Along the Internal Housing Walls of Aero Engine Bearing Chambers,” ASME Paper No. 97-GT-261.
3. Two-Phase Air/Oil Flow in Aero-Engine Bearing Chambers-Assessment of an Analytical Method for the Internal Wall Heat Transfer;Glahn;Int. J. Rotating Mach.
4. Internal Bearing Chamber Wall Heat Transfer as a Function of Operating Conditions and Chamber Geometry;Busam;ASME J. Eng. Gas Turbines Power
5. Two-Phase Air/Oil Flow in Aero Engine Bearing Chambers: Characterization of the Oil Film Flow;Glahn;ASME J. Eng. Gas Turbines Power
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