[1] Wittig S, Glahn A, Himmelsbach J. Influence of high rotational speeds on heat transfer and oil film thickness in aero-engine bearing. Journal of Engineering for Gas Turbines and Power, 1994, 116(2): 395-401.[2] Busam S, Glahn A, Wttig S. Internal bearing chamber wall heat transfer as a function of operating conditions and chamber geometry. Journal of Engineering for Gas Turbines and Power, 2000, 122(4): 314-320.[3] Glahn A, Busam S, Wittig S. Local and mean heat transfer coefficients along the internal housing walls of aero engine bearing chambers. ASME Paper No.97-GT-261, 1997.[4] Glahn A, Kurreck M, Willmann M, et al. Feasibility study on oil droplet flow investigations inside aero engine bearing chambers-PDPA techniques in combination with numerical approaches. Journal of Engineering for Gas Turbines and Power, 1996, 118(4): 749-755.[5] Glahn A, Wittig S. Two-phase air/oil flow in aero engine bearing chambers: characterization of oil film flows. Journal of Engineering for Gas Turbines and Power, 1996, 118(3): 578-583.[6] Glahn A, Wittig S. Two-phase air/oil flow in aero-engine bearing chambers-assessment of an analytical prediction method for the internal wall heat transfer. International Journal of Rotating Machinery, 1999, 5(3): 155-165.[7] Gorse P, Busam S, Dullenkopf K. Influence of operating condition and geometry on the oil film thickness in aeroengine bearing chambers. Journal of Engineering for Gas Turbines and Power, 2006, 128(1): 103-110.[8] Farrall M, Simmons K, Hibberd S, et al. A numerical model for oil film flow in an aeroengine bearing chamber and comparison to experimental data. Journal of Engineering for Gas Turbines and Power, 2006, 128(1): 111-117.[9] Farrall M, Hibberd S, Simmons K, et al. Prediction of air/oil exit flows in a commercial aero-engine bearing chamber. Proceedings of the Institution of Mechanical Engineers Part G: Journal of Aerospace Engineering, 2006, 220(3): 197-202.[10] Farrall M, Hibberd S, Simmons K. The effect of initial injection conditions on the oil droplet motion in a simplified bearing chamber. Journal of Engineering for Gas Turbines and Power, 2008, 130(1): 12501-12507.[11] Wang C, Morvan H P, Hibberd S, et al. Thin film modelling for aero-engine bearing chambers. Turbine Technical Conference and Exposition, 2011: 277-286.[12] Chen G D, Sun H C, Wang J. Research into configuration and flow of wall oil film in bearing chamber based on droplet size distribution. Chinese Journal of Aeronautics, 2011, 24(3): 355-362.[13] Ibrahim E A, Yang H Q, Przekwas A J. Modeling of spray droplets deformation and breakup. Journal of Propulsion and Power, 1993, 9(4): 651-654.[14] Chen B, Chen G D, Sun H C, et al. Effect of oil droplet deformation on its deposited characteristics in an aeroengine bearing chamber. Proceedings of the Institution of Mechanical Engineers Part G: Journal of Aerospace Engineering (in press).[15] Wu Z N. Prediction of the size distribution of secondary ejected droplets by crown splashing of droplets impinging on a solid wall. Probabilistic Engineering Mechanics, 2003, 18(3): 241-249.[16] Bai C X, Rusche H, Gosman A D. Modeling of gasoline spray impingement. Atomization and Sprays, 2002, 12(1-3): 1-27.[17] Bai C X, Gosman A D. Development of a methodology for spray impingement simulation. SAE Paper, 1995, 950283: 69-87.[18] Glahn A, Busam S, Blair M F, et al. Droplet generation by disintegration of oil films at the rim of a rotating disk. Journal of Engineering for Gas Turbines and Power, 2002, 124(1): 117-124. |