Philosophical Transactions of the Royal Society A: Mathematical, Physical and Engineering Sciences

    Considerable progress in development and application of computational fluid dynamics (CFD) for aeroengine internal flow systems has been made in recent years. CFD is regularly used in industry for assessment of air systems, and the performance of CFD for basic axisymmetric rotor/rotor and stator/rotor disc cavities with radial throughflow is largely understood and documented. Incorporation of three-dimensional geometrical features and calculation of unsteady flows are becoming commonplace. Automation of CFD, coupling with thermal models of the solid components, and extension of CFD models to include both air system and main gas path flows are current areas of development. CFD is also being used as a research tool to investigate a number of flow phenomena that are not yet fully understood. These include buoyancy-affected flows in rotating cavities, rim seal flows and mixed air/oil flows. Large eddy simulation has shown considerable promise for the buoyancy-driven flows and its use for air system flows is expected to expand in the future.

    References

    • Armstrong, I. & Edmunds, T. E. 1989 Fully automatic analysis in the industrial environment. In Proc. 2nd Int. Conf. on Quality Assurance and Standards in Finite Element Analysis, NAFEMS. Google Scholar
    • Bohn D, Bonhoff H, Schonenborn H& Wilhelmi HValidation of a numerical model for the coupled simulation of fluid flow and diabatic walls with application to film-cooled turbine blades. VDI-Berichte. 1196, 1995a259–272. Google Scholar
    • Bohn D, Deuker E, Emunds R& Gorzelitz VExperimental and theoretical investigations of heat transfer in closed gas-filled rotating annuli. ASME J. Turbomach. 117, 1995b175–183. Crossref, ISIGoogle Scholar
    • Bohn, D., Ren, J. & Kusterer, K. 2003a Conjugate heat transfer analysis for film cooling configurations with different hole geometries. In Proc. ASME Turbo Expo. Paper 2003-GT-38369. Google Scholar
    • Bohn, D., Heuer, T. & Kusterer, K. 2003b Conjugate flow and heat transfer investigation of a turbo charger. Part I: numerical results. In Proc. ASME Turbo Expo. Paper 2003-GT-38445. Google Scholar
    • Bohn, D., Moritz, N. & Wolff, M. 2003c Conjugate flow and heat transfer investigation of a turbo charger. Part II: experimental results. In Proc. ASME Turbo Expo. Paper 2003-GT-38449. Google Scholar
    • Boudet J, Autef V.N.D, Chew J.W, Hills N.J& Gentilhomme O. 2005Numerical simulation of rim seal flows in axial turbines. Aeronaut. J. 109, 373–383. ISIGoogle Scholar
    • Boudet, J., Chew, J. W. & Hills, N. J. 2006 Numerical simulation of the flow interaction between turbine main annulus and disc cavities. In Proc. ASME Turbo Expo. Paper GT2006-90307. Google Scholar
    • Cao, C., Chew, J. W., Millington, P. R. & Hogg, S. 2003 Interaction of rim seal and annulus flows in an axial flow turbine. In Proc. ASME Turbo Expo. Paper GT2003-38368. (Also ASME J. Eng. for Gas Turbines and Power, 126, pp. 786–793.). Google Scholar
    • Cherry, D., Wadia, A., Beacock, R., Subramanian, M. & Vitt, P. 2005 Analytical investigation of low pressure turbine with and without endwall gaps seals and clearance features. In Proc. ASME Turbo Expo. Paper GT2005 68492. Google Scholar
    • Chew J.W. 1984Development of a computer program for the prediction of flow and heat transfer in rotating cavities. Int. J. Num. Methods Fluids. 4, 667–683.doi:10.1002/fld.1650040706. . Crossref, ISIGoogle Scholar
    • Chew, J. W. 1990 Prediction of rotating disc flow and heat transfer in gas turbine engines. In Proc. 3rd Int. Symp. Transport Phenomena and Dynamics of Rotating Machinery, pp. 145–160. Honolulu, HI: Hemisphere Publishers. Google Scholar
    • Chew, J. W. 1996 Analysis of the oil film on the inside surface of an aero-engine bearing chamber housing. In ASME Gas Turbine Conf. Paper 96-GT-300. Google Scholar
    • Chew, J. W. & Vaughan, C. M. 1988 Numerical predictions for the flow induced by an enclosed rotating disc. In ASME Gas Turbine and Aeroengine Cong. Paper 88-GT-127. Google Scholar
    • Chew J.W, Dadkhah S& Turner A.B. 1992Rim sealing of rotor–stator wheelspaces in the absence of external flow. ASME J. Turbomach. 124, 306–315. Google Scholar
    • Chew, J. W., Taylor, I. J. & Bonsell, J. J. 1996 CFD developments for turbine blade heat transfer. In Proc. 3rd Int. Conf. on Reciprocating Engines and Gas Turbines, IMechE. Google Scholar
    • Chew, J. W., Hills, N. J., Khalatov, S., Scanlon, T. & Turner A. B. 2003 Measurement and analysis of flow in a pre-swirled cooling air delivery system. In Proc. ASME Turbo Expo. Paper GT-2003-38084. Google Scholar
    • Chew, J. W., Hills, N. J., Khalatov, S., Scanlon, T. & Turner A. B. 2003 Measurement and analysis of flow in a pre-swirled cooling air delivery system. In Proc. ASME Turbo Expo. Paper GT-2003-38084. Google Scholar
    • Ciampoli, F., Chew, J. W., Shahpar, S. & Willocq, E. 2006 Automatic optimisation of pre-swirl nozzle design. Proc. ASME Turbo Expo, Paper GT2006-90249. (Also 2007 ASME J. Engng Gas Turbines and Power, 129, 387–393.). Google Scholar
    • Crumpton P.I, Muller J.-D& Giles M.B. 2002Edge based multigrid schemes and preconditioning for hybrid grids. AIAA J. 40, 1954–1960. CrossrefGoogle Scholar
    • Daily J.W& Nece R. 1960Chamber dimension effects on induced flow and frictional resistance of enclosed rotating disks. ASME J. Basic Eng. 82, 217–232. CrossrefGoogle Scholar
    • Dawes, W. N. 2006 Eliminating serial bottlenecks not just in the flow solving but also in the mesh generation and geometry management. In Proc. ASME Turbo Expo. Paper GT-2006-90620. Google Scholar
    • Denecke, J., Schramm, V., Dullenkopf, K., Bauer, H.-J., Klingsporn, M., Hein, S. & Peitsch, D. 2006 Advanced hydraulic seal design for high temperature environments. In Proc. ASME Turbo Expo. Paper GT2006-90651. Google Scholar
    • Eastwick, C., Bertin, L. & Johnson, G. 2006 The effect of obstacles in a liquid film. In Proc. ASME Turbo Expo. Paper GT2006-90520. Google Scholar
    • Farrall, M., Hibberd, S. & Simmons, S. 2003 Modelling oil droplet/film interaction in an aero-engine bearing chamber. In ICLASS Conf., Sorento. Google Scholar
    • Farrall, M., Simmons, S., Hibberd, S. & Gorse, P. 2004 Modelling oil droplet/film interaction in an aero-engine bearing chamber and comparison with experimental data. In Proc. ASME Turbo Expo. Paper GT-2004-53698. Google Scholar
    • Geis, T., Dittmann, M. & Dullenkopf, K. 2003. Cooling air temperature reduction in a direct transfer preswirl system. In Proc. ASME Turbo Expo. Paper GT-2003-38231. Google Scholar
    • Gentilhomme, O. J. P. 2004 Turbine rim seal ingestion. DPhil thesis, University of Sussex. Google Scholar
    • Glahn, A. & Wittig, S. 1995 Two-phase air/oil flow in aero engine bearing chambers—Characterization of oil film flows. In ASME Turbomachinery Conf. Paper 95-GT-114. Google Scholar
    • Glahn, A., Kurreck, M., Willmann, M. & Wittig, S. 1995 Feasibility study on oil droplet flow investigations inside aero engine bearing chambers. In ASME Turbomachinery Conf. Paper 95-GT-100. Google Scholar
    • Glahn A, Busam S, Blair M.F, Allard K.L& Wittig S. 2002Droplet generation by disintegration of oil films at the rim of a rotating disk. ASME J. Eng. Gas Turbines Power. 124, 117–124.doi:10.1115/1.1400753. . Crossref, ISIGoogle Scholar
    • Glahn A, Blair M.F, Allard K.L, Busam S, Schäfer O& Wittig SDisintegration of oil jets emerging from axial passages at the face of a rotating cylinder. ASME J. Eng. Gas Turbines Power. 125, 2003a1003–1010.doi:10.1115/1.1586310. . Crossref, ISIGoogle Scholar
    • Glahn A, Blair M.F, Allard K.L, Busam S, Schäfer O& Wittig SDisintegration of oil films emerging from radial holes in a rotating cylinder. ASME J. Eng. Gas Turbines Power. 125, 2003b1011–1020.doi:10.1115/1.1586311. . Crossref, ISIGoogle Scholar
    • Gorse, P., Willenborg, K., Busam, S., Ebner, J., Dullenkopf, K. & Wittig, S. 2003 3D-LDA measurements in an aero-engine bearing chamber. In Proc. ASME Turbo Expo. Paper GT2003-38376. Google Scholar
    • Gosman, A. D., Koosinlin, M. L., Lockwood, F. C. & Spalding, D. B. 1976 Transfer of heat in rotating systems. In ASME Turbomachinery Conf. Paper 76-GT-25. Google Scholar
    • Heselhaus A, Vogel D.T& Krain HCoupling of 3D Navier–Stokes external flow calculations and internal 3D heat conduction calculations for cooled turbine blades. AGARD, heat transfer and cooling in gas turbines1994pp. 40.1–40.9. Google Scholar
    • Hills N.J. 2007Achieving high parallel performance for an unstructured unsteady turbomachinery CFD code. Aeronaut. J. (Special edition). 111, 185–194. Crossref, ISIGoogle Scholar
    • Hirt C.W& Nichols B.D. 1981Volume of fluid (VOF) method for the dynamics of free boundaries. J. Comput. Phys. 39, 201–225.doi:10.1016/0021-9991(81)90145-5. . Crossref, ISIGoogle Scholar
    • Ho, Y. H., Athavale, M. M., Forry, J. M., Hendricks, R. C. & Steinetz, B. M. 1996 Numerical simulation of secondary flow in gas turbine and disc cavities including conjugate heat transfer. In ASME Turbomachinery Conf. Paper 96-GT-67. Google Scholar
    • Iacovides H& Chew J.W. 1993Prediction of heat transfer in rotating disc systems. Int. J. Heat Fluid Flow. 14, 146–154.doi:10.1016/0142-727X(93)90022-F. . Crossref, ISIGoogle Scholar
    • Illingworth, J., Hills, N. & Barnes, C. 2005 3D fluid–solid heat transfer coupling of an aero-engine preswirl system, In Proc. ASME Turbo Expo. Paper 2005-GT-68939. Google Scholar
    • Isaac Newton Institute for Mathematical Sciences 1999 Workshop on future strategies towards understanding and prediction of turbulent systems. Lecture notes issued by INIMS. Cambridge, UK: University of Cambridge. Google Scholar
    • Jameson, A. & Caughey, D. A. 2001 How many steps are required to solve the Euler equations of steady compressible flow: in search of a fast solution algorithm. AIAA Paper 2001-2673. Google Scholar
    • Johnson, B. V., Jakoby, R., Bohn, D. E. & Cunat, D. 2006 A method for estimating the influence of time-dependent vane and blade pressure fields on turbine rim seal ingestion. In Proc. ASME Turbo Expo. Paper GT2006-90853. Google Scholar
    • Karypsis G& Kumar V. 1999A fast and high quality scheme for partitioning irregular graphs. SIAM J. Sci. Comput. 20, 359–392.doi:10.1137/S1064827595287997. . Crossref, ISIGoogle Scholar
    • King, M. P., Wilson, M. & Owen, J. M. 2005 Rayleigh–Benard convection in open and closed rotating cavities. In Proc. ASME Turbo Expo. Paper GT2005-68948. Google Scholar
    • Kirkpatrick A.T& Bohn M. 1986An experimental investigation of mixed cavity convection in the high Rayleigh number regime. Int. J. Heat Mass Transfer. 29, 69–82.doi:10.1016/0017-9310(86)90035-9. . Crossref, ISIGoogle Scholar
    • Klingsporn, M. 2004 Advanced transmission and oil system concepts for modern aero-engines. In Proc. ASME Turbo Expo. Paper GT2004-53578. Google Scholar
    • Lee, C. W., Palma, P. C., Simmons, K. & Pickering, S. J. 2004 Comparison of CFD and PIV data for the airflow in an aero-engine bearing chamber. In Proc. ASME Turbo Expo. Paper GT2004-53281. Google Scholar
    • Lewis, P., Wilson, M., Lock, G. & Owen, J. M. 2006 Physical interpretation of flow and heat transfer in pre-swirl systems. In Proc. ASME Turbo Expo. Paper GT-2006-90132. Google Scholar
    • Li, H. & Kassab, A. J. 1994 A coupled FVM/BEM approach to conjugate heat transfer in turbine blades. AIAA Paper 94-1981. Google Scholar
    • Long C.A& Tucker P.G. 1994Numerical computation of laminar flow in a heated rotating cavity with an axial throughflow of air. Int. J. Num. Methods Heat Fluid Flow. 4, 347–365.doi:10.1108/EUM0000000004043. . Crossref, ISIGoogle Scholar
    • Long, C. A., Alexiou, A. & Smout, P. D. 2003 Heat transfer in H.P. compressor gas turbine internal air systems: measurements from the peripheral shroud of a rotating cavity with axial throughflow. In HEFAT2003, 2nd Int. Conf. on Heat Transfer, Fluid Mechanics and Thermodynamics. Paper LC1. Google Scholar
    • Lumley J.LPrediction methods in turbulence, workshop on future strategies towards understanding and prediction of turbulent systems. 1999Cambridge, UK:Isaac Newton Institute. Google Scholar
    • May N.E, Chew J.W& James P.W. 1994Calculation of turbulent flow for an enclosed rotating cone. ASME J. Turbomach. 116, 548–554. Crossref, ISIGoogle Scholar
    • Meierhofer B. & Franklin C. J. 1981 An investigation of preswirled cooling airflow to a turbine disc by measuring the air temperature in the rotating channels. In ASME Turbomachinery Conf. Paper 81-GT-132. Google Scholar
    • Mirzamoghadam, A. V. & Xiao, Z. 2000 Flow and heat transfer in an industrial rotor-stator rim sealing cavity. In ASME Turbo Expo. Paper 2000-GT-285. Google Scholar
    • Monico, R. D. & Chew, J. W. 1992 Modelling the thermal behaviour of turbomachinery discs and casings. In AGARD PEP Symp. Heat Transfer and Cooling in Gas Turbines, pp. 24.1–24.9. Google Scholar
    • Mulder W. 1989A new approach to convection problems. J. Comp. Phys. 83, 303–323.doi:10.1016/0021-9991(89)90121-6. . Crossref, ISIGoogle Scholar
    • Owen J.M& Rogers R.H vol. 11989Taunton, MA; New York, NY:Research Studies Press; Wiley. Google Scholar
    • Owen J.M& Rogers R.H vol. 21995Taunton, MA; New York, NY:Research Studies Press; Wiley. Google Scholar
    • Owen, J. M., Abrahamsson, H. & Lindblad, K. 2006 Buoyancy-induced flow in open rotating cavities. In Proc. ASME Turbo Expo. Paper GT-2006-91134. Google Scholar
    • Pierce N.A& Giles M. 1997Preconditioned multigrid methods for compressible flow calculations on stretched grids. J. Comp. Phys. 136, 425–445.doi:10.1006/jcph.1997.5772. . Crossref, ISIGoogle Scholar
    • Pope S.B. 2004Ten questions concerning the large-eddy simulation of turbulent flows. New J. Phys. 6, 35doi:10.1088/1367-2630/6/1/035. . Crossref, ISIGoogle Scholar
    • Rigby, D. L. & Lepicovsky, J. 2001 Conjugate heat transfer analysis of internally cooled configurations. In Proc. ASME Turbo Expo. Paper 2001-GT-0405. Google Scholar
    • Rosic, B., Denton, J. D. & Pullan, G. 2005 The importance of shroud leakage modelling in multistage turbine flow calculations. In Proc. ASME Turbo Expo. Paper GT2005-68459. Google Scholar
    • Rossow, C.-C., 2006. Toward efficient computation of compressible and incompressible flows. AIAA Paper 2006-3522. Google Scholar
    • Scanlon, T., Wilkes, J., Bohn, D. & Gentilhomme, O. 2004 A simple method of estimating ingestion of annulus gas into a turbine rotor stator cavity in the presence of external pressure gradients. In Proc. ASME Turbo Expo. Paper GT2004-53097. Google Scholar
    • Shahpar, S., Giacche, D. & Lapworth L. 2003 Multi-objective design and optimisation of bypass outlet guide vanes. In Proc. ASME Turbo Expo. Paper GT2003-38700. Google Scholar
    • Smout, P. D., Chew, J. W. & Childs, P. R. N. 2002 ICAS-GT: a European collaborative research programme on internal cooling air systems for gas turbines. In Proc. ASME Turbo Expo. Paper GT-2002-30479. Google Scholar
    • Snowsill, G. & Young, C. 2006 The application of CFD to underpin the design of gas turbine pre-swirl systems. In Proc. ASME Turbo Expo. Paper GT-2006-90443. Google Scholar
    • Staub, F. W. 1992 Rotor cavity flow and heat transfer with inlet swirl and radial outflow of cooling air. In ASME Turbomachinery Conf. Paper GT-92-378. Google Scholar
    • Sun, Z, Kilfoil, A., Chew, J. W. & Hills, N. J. 2004 Numerical simulation of natural convection in stationary and rotating cavities. In Proc. ASME Turbo Expo. Paper GT2004-53528. Google Scholar
    • Sun, Z., Lindblad, K., Chew, J. W. & Young, C. 2006 LES and RANS investigations into buoyancy-affected convection in a rotating cavity with a central axial throughflow. Proc. ASME Turbo Expo, Paper GT2006-90251. (Also 2007 ASME J. Engng Gas Turbines and Power, 129, 318–325.). Google Scholar
    • Van Wachen B.G.M& Almstedt A.E. 2003Methods for multiphase computational fluid dynamics. Chem. Eng. J. 96, 81–98.doi:10.1016/j.cej.2003.08.025. . Crossref, ISIGoogle Scholar
    • Verdicchio, J., Chew, J. W. & Hills, N. J. 2001 Coupled fluid/solid heat transfer computation for turbine discs. In Proc. ASME Turbo Expo. Paper 2001-GT-205. Google Scholar
    • Virr G.P, Chew J.W& Coupland J. 1994Application of computational fluid dynamics to turbine disc cavities. ASME J. Turbomach. 116, 701–708. Crossref, ISIGoogle Scholar
    • Wellbourn, S. R. & Okiishi, T. H. 1998 The influence of shrouded stator cavity flows on multistage compressor performance. In ASME Gas Turbine Expo. Paper 98-GT-12. Google Scholar
    • Wilson M, Pilbrow R& Owen J.M. 1997Flow and heat transfer in a pre-swirl rotor-stator system. ASME J. Turbomach. 119, 363–373. Crossref, ISIGoogle Scholar
    • Wittig S, Glahn A& Himmelsbach J. 1994Influence of high rotational speeds on heat transfer and oil film thickness in aero engine bearing chambers. ASME J. Eng. Gas Turbines Power. 116, 395–401. Crossref, ISIGoogle Scholar
    • Wong, L.-S. 2002 Flow and heat transfer in rotationally induced buoyancy flow. DPhil thesis, University of Sussex. Google Scholar
    • Yamada Y& Ito M. 1975On the frictional resistance of enclosed rotating cones. Bull. JSME. 18, 1026. CrossrefGoogle Scholar
    • Yamada Y& Ito M. 1979Frictional resistance of enclosed rotating cones with superposed throughflow. ASME J. Fluids Eng. 101, 259. Crossref, ISIGoogle Scholar
    • Young, C. & Chew, J. W. 2005 Evaluation of the volume of fluid modelling approach for simulation of oil/air system flows. In Proc. ASME Turbo Expo. Paper GT2005-68861. Google Scholar