Suo, M., 1978, “Turbine Cooling,” "Aero-Thermodynamics of Aircraft Gas Turbine Engines", G.C.Oates ed.,Air Force Aero Propulsion Laboratory Report AFAPL-TR-78-52.
Campbell, D. A., 1978, “Gas Turbine Disc Sealing System Design,” Report No. AGARD-CP-237, p. 18.
Smout, P. D., Chew, J. W., and Childs, P. R. N., 2002, “ICAS-GT: A European Collaborative Research Programme on Internal Cooling Air Systems for Gas Turbines,” ASME Paper No. GT-2002-30479.
Bohn, D. E., Decker, A., Ma, H., and Wolff, M., 2003, “Influence of Sealing Air Mass Flow on the Velocity Distribution In and Inside the Rim Seal of the Upstream Cavity of a 1.5-Stage Turbine,” ASME Paper No. GT2003-38459.
Jakoby, R., Zierer, T., Lindblad, K., Larssson, J., deVito, L., Bohn, D. E., Funcke, J., and Decker, A., 2004, “Numerical Simulation of the Unsteady Flow Field in an Axial Gas Turbine Rim Seal Configuration,” ASME Paper No. GT2004-53829.
Johnson, B. V., Mack, G. J., Paolillo, R. E., and Daniels, W. A., 1994, “Turbine Rim Seal Gas Path Flow Ingestion Mechanisms,” AIAA Paper No. AIAA 94-2703.
Bayley, F. J., and Owen, J., 1970, “The Fluid Dynamics of a Shrouded Disk System With a Radial Outflow of Coolant,” ASME J. Eng. Power, 92 , pp. 335–341.
Phadke, U. P., and Owen, J. M., 1983, “An Investigation of Ingress for an ‘Air-Cooled’ Shrouded Rotating Disk System With Radial Clearance Seals,” ASME J. Eng. Power, 105 , pp. l78–183.
Owen, J. M., and Rogers, R. H., 1989, "Flow and Heat Transfer in Rotating Disc Systems, Volume 1: Rotor-Stator Systems", Wiley, New York.
Daniels, W. A., Johnson, B. V., Graber, D. J., and Martin, R. J., 1992, “Rim Seal Experiments and Analysis for Turbine Applications,” ASME J. Turbomach., l14 , pp. 426–432.
Chew, J. W., 1989, “A Theoretical Study of Ingress for Shrouded Rotating Disc Systems With Radial Outflow,” ASME J. Turbomach.
[CrossRef]113 , pp. 91–97.
Johnson, B. V., 1975, “A Turbulent Diffusion Model for Turbine Rim Seal Cavity Seals,” UTRC Report No. 75-17.
Graber, D. J., Daniels, W. A., and Johnson, B. V., 1987, “Disk Pumping Test, Final Report for Period August 1983 to February 1987,” Air Force Wright Aeronautical Laboratories, Report No. AFWAL-TR-87-2050.
Abe, T., Kikuchi, J., and Takeuchi, H., 1979, “An Investigation of Turbine Disk Cooling: Experimental Investigation and Observation of Hot Gas Flow Into a Wheel Space,” 13th CIMAG Congress , Vienna, Paper No. GT30.
Green, T., and Turner, A. B., 1994, “Ingestion Into the Upstream Wheelspace of an Axial Turbine Stage,” ASME J. Turbomach.
[CrossRef], 116 , pp. 327–332.
Chew, J. W., Green, T., and Turner, A. B., 1994, “Rim Sealing of Rotor-Stator Wheelspaces in the Presence of External Flow,” ASME Paper No. 94-GT-16.
Hills, N. J., Chew, J. W., Green, T., and Turner, A. B., 1997, “Aerodynamics of Turbine Rim-Seal Ingestion,” ASME Paper No. 97-GT-268.
Bohn, D., and Wolf, M., 2003, “Improved Formulation to Determine Minimum Sealing Flow—Cw, min—for Different Sealing Configurations,” ASME Paper No. GT2003-38465.
Scanlon, T., Wilkes, J., Bohn, D., and Gentilhomme, O., 2004, “A Simple Method for Estimating Ingestion of Annulus Gas Into a Turbine Rotor Stator Cavity in the Presence of External Pressure Variations,” ASME Paper No. GT2004-53097.
Gentilhomme, O., Hills, N. J., Turner, A. B., and Chew, J. W., 2002, “Measurement and Analysis of Ingestion Through a Rim Seal,” ASME Paper No. GT-2002-30481.
Roy, R. P., Feng, J., Narzary, D. Saurabh, P., and Paolillo, R. E., 2004, “Experiments on Gas Ingestion Through Axial-Flow Turbine Rim Seals,” ASME Paper No. GT2004-53394.
Bohn, D., Rudzinski, B., Suerken, N., and Gaertner, W., 2000, “Experimental and Numerical Investigation of the Influence of Rotor Blades on Hot Gas Ingestion into the Upstream Cavity of an Axial Turbine Stage,” ASME Paper No. 2000-GT-284.
Foerster, I., Martens, E., Friedl, W.-H., and Peitsch, D., 2001, “Numerical Study of Hot Gas Ingestion Into an Engine Type High-Pressure Turbine Rotor-Stator Cavity,” ASME Paper No. 2001-GT-0114.
Okita, Y., Nishiura, M., Yamawaki, S., and Hironaka, Y., 2004, “A Novel Cooling Method for Turbine Rotor-Stator Rim Cavities Affected by Mainstream Ingress,” ASME Paper No. GT2004-53016.
Bayley, F. J., 1999, “Flows and Temperatures in Compressor and Turbine Wheelspaces,” Proc. Inst. Mech. Eng., Part C: J. Mech. Eng. Sci., 213 , pp. 451–460.
Bohn, D., Rudzinski, B., and Suerken, N., 1999, “Influence of Rim Seal Geometry on Hot Gas Ingestion Into the Upstream Cavity of an Axial Turbine Stage,” ASME Paper No. 99-GT-248.
Bohn, D. E., Decker, A., and Ohlendorf, N., 2006, “Influence of a Radial and Axial Rim Seal Geometry on Hot Gas Ingestion into the Upstream Cavity of a 1.5 -Stage Turbine,” ASME Paper No. GT2006-90453.
Dring, R. P., Joslyn, H. J., Hardin, L. W., and Wagner, J. H., 1982, “Turbine Rotor-Stator Interactions,” ASME J. Eng. Power, 104 , pp. 729–742.
Feiereisen, J. M., Paolillo, R. E., and Wagner, J., 2000, “UTRC Turbine Rim Seal Ingestion and Platform Cooling Experiments,” AIAA Report No. 2000-3371.
Vaughan, C. M., 1986, “A Numerical Investigation Into the Effect of an External Flow Field on the Sealing of a Rotor-Stator Cavity,” Ph.D. thesis, University of Sussex.
Chew, J. W., Dadkhah, S., and Turner, A. B., 1991, “Rim Sealing of Rotor-Stator Wheelspaces in the Absence of External Flow,” ASME Paper No. 91-GT-33.
Wang, C.-Z., Johnson, B. V., Cloud, D. E., Paolillo, R. E., Vashist, T. K., and Roy, R., 2006, “Rim Seal Ingestion Characteristics for Axial Gap Rim Seals in a Close-Spaced Turbine Stage From a Numerical Simulation,” ASME Paper No. GT2006-90965.