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Sumanta Acharya 387 37. K. Hermanson, S. Kern, G. Picker, and S. Parneix, “Predictions of External Heat Transfer For Turbine Vanes and Blades With Secondary Flowfields,” ASME Proc. Turbo Expo, GT-2002-30206, 2002. 38. See note 33 above. 39. A. Yamamoto, “Production and Development of Secondary Flows and Losses in Two Types of Straight Turbine Cascades: Part 1- A Stator Case,” ASME Tran. J. Turbomachinery 109 (1987): 186-193;R.P. Roy, K.D. Squires, M. Gerendas, S. Song, W.J. Howe and A. Ansari, “Flow and Heat Transfer at the Hub Endwall of Inlet Vane Passages- Experiments and Simulations,” ASME Proc. Turbo Expo, 2000-GT-198, 2000. 40. See note 3 above. 41. See note 3 above. 42. See note 3 above. 43. See note 13 above. 44. See note 13 above. 45. R.G. Dominy and S.C. Harding, “An Investigation of Secondary Flows in Nozzle Guide Vanes,” AGARD Conf. Proc. No. 469, Secondary Flows in Turbomachines (1990): 7.1-7.15. 46. See note 3 above (Gallus). 47. M.V. Hoyningen-Huene, W. Frank, and A.R. Jung, “Three-Dimensional Time-Resolved Flow Field in the First and Last Turbine Stage of a Heavy Duty Gas Turbine, Part I: Secondary Flow Field,” ASME Proc. Turbo Expo, 2000-GT-0438, 2000. 48. J. Zeschky and H.E. Gallus, “Effects of Stator Wakes and Spanwise Nonuniform Inlet Conditions on the Rotor Flow of an Axial Turbine Stage,” ASME Tran. J. Turbomachinery 115 (1993): 128-136. 49. H. Sauer, R. Müller, and K. Vogeler, “Reduction of Secondary Flow Losses in Turbine Cascades by Leading Edge Modifications at the Endwall,” ASME Tran. J. Turbomachinery 123 (2001): 207-213; G. A. Zess and K.A. Thole, “Computational Design and Experimental Evaluation of Using a Leading Edge Fillet on a Gas Turbine Vane,” ASME Proc. Turbo Expo, GT-2001-0404, 2001; A.T. Lethander, K.A. Thole, G. Zess, and J. Wagner, “Ortimizing the Vane- Endwall Junction to Reduce Adiabatic Wall Temperatures in a Turbine Vane Passage,” ASME Proc. Turbo Expo, GT2003-38939, 2003; S. Becz, M.S. Majewski, and L.S. Langston, “Leading Edge Modification Effects on Turbine Cascade Endwall Loss,” ASME Proc. Turbo Expo, GT-2003-38898, 2003;S. Becz, M.S. Majewski, and L.S. Langston, “An Experimental Investigation of Contoured Leading Edges for Secondary Flow Loss Reduction,” ASME Proc. Turbo Expo, GT-2004-53964, 2004; also see notes 22 and 25 above. 50. See notes 22 and 25 above. 51. See note 21 above. 52. See note 25 above. 53. See note 49 above. 54. See note 49 above (Zess). 55. S.W. Burd and T.W. Simon, “Flow Measurements in a Nozzle Guide Vane Passage With a Low Aspect Ratio and Endwall Contouring,” ASME Proc. Turbo Expo, 2000-GT-0213, 2000; T.I-P Shih, Y.-L Lin, and T.W. Simon, “Control of Secondary Flows in a Turbine Nozzle Guide Vane by Endwall Contouring,” ASME Proc. Turbo Expo, 2000-GT-0556, 2000; V. Dossena, A. Perdichizzi, and M. Savini, “The Influence of Endwall Contouring on the Performance of a Turbine Nozzle Guide Vane,” ASME Tran. J. Turbomachinery 121(1999): 200-208; F.C. Kopper, R. Milano, and M. Vanco, “Experimental Investigation of Endwall Profiling in a Turbine Vane Cascade,” AIAA Journal, AIAA 80-1089R 19, No. 8 ( August 1981). 56. S. Acharya, “Eendwall Cooling With Endwall Contouring and Leading Edge Fillet,” Smi-annual Report Submiited to UTSR, South Carolina, Project No. 02-01-SR098, June 2003-December 2003; D.E. Bohn, K. Kusterer, N. Sürken, and F. Kreitmeler, “Influence of Endwall Contouring in Axial Gaps on the Flow Field in a Four-Stage Turbine,” ASME Proc. Turbo Expo, 2000-GT-472, 2000; L.P. Timko, “Energy Efficient Engine High Pressure Turbine Component Test Performance Report,” Contract Report for NASA, Report No. NASA CR-168289; also see note 55 above (Shih). 57. See note 55 above (Burd). 58. See note 55 above (Dossena). 59. Ibid. 60. See note 3 above (Boletis). 61. See note 55 above (Dossena). 62. R. Gustafson, G.I. Mahmood, and S. Acharya, “Control of Secondary Flows in a Low Speed Blade Cascade with a Non- axisymmetric 3-D Endwall,” in preparation for the ASME Trans J. Turbomachinery. 63. N. W. Harvey, M.G. Rose, M.D. Taylor, S. Shahpar, J. Hartland, and D.G. Gregory-Smith, “Nonaxisymmetric Turbine End Wall Design: Part I- Three-Dimensional Linear Design System,” ASME Tran. J. Turbomachinery 122 (2000): 278-285; J.C. Hartland, D.G. Gregory-Smith, and M.G. Rose, “Non-axisymmetric Endwall Profiling in a Turbine Rotor Blade,” ASME Proc. Turbo Expo, 98-GT-525, 1998. 64. G. Ingram, D.G. Gregory-Smith, M. Rose, N. Harvey, and G. Brennan, “The Effect of End-wall Profiling on Secondary Flow and Loss Development in a Turbine Cascade,” ASME Proc. Turbo Expo, GT-2002-30339, 2002; J.C. Hartland, D.G. Gregory-Smith, N.W. Harvey, and M.G. Rose, “Nonaxisymmetric Turbine End Wall Design: Part II- ExperimentalPDF Image | Turbine Blade Aerodynamics
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