Improving Turbine Efficiency by Combining the Effects of Rim Seals and End-Wall Contours in the Presence of Purge Flow

Engineering

1. Turbine 100%
2. Secondary Flow 91%
3. Stages 90%
4. Measurement 86%
5. Vortex 83%
6. Rotors 62%
7. Flow Field 60%
8. Flow Structure 47%
9. Gas Turbine 46%
10. Horseshoe Vortex 43%
11. Design 39%
12. Pressure Side 39%
13. Facilities 37%
14. Axisymmetric 32%
15. Suction Side 31%
16. Seals 31%
17. Mainstream Flow 30%
18. Blade Passage 30%
19. Single Stage Turbine 28%
20. Engine 23%
21. Temperature 22%
22. Computational Fluid Dynamics 21%
23. Efficiency 20%
24. Turbine Efficiency 18%
25. Blade Row 18%
26. Momentum Flux 18%
27. Fluid 18%
28. Borescope 18%
29. Stator 18%
30. Performance 18%
31. Loss 17%
32. Disc Turbine 15%
33. Leading Edge 13%
34. Guide Vane 12%
35. Application 12%
36. Nozzle 12%
37. Measurement System 12%
38. Turbomachinery 12%
39. Static Pressure 12%
40. Pressure Field 12%
41. Fluid Dynamics 12%
42. Rotational 12%
43. Periphery 12%
44. Radius 12%
45. Velocity 11%
46. Velocity Field 10%
47. Convection 9%
48. Cycle Efficiency 8%
49. Flowrates 8%
50. Particle Image Velocimetry 7%
51. Measures 7%
52. Field Measurement 7%
53. Flow Condition 7%
54. Test Rig 7%
55. Environment 7%
56. Forming 7%
57. Suction Surface 7%
58. Aerodynamics 7%
59. Experiments 7%
60. Dataset 6%
61. Experimental Technique 6%
62. Quantitative Analysis 6%
63. Induced Velocity 6%
64. High Quality 6%
65. Research 6%
66. Quality Data 6%
67. Main Flow 6%
68. Boundary Condition 6%
69. Good Agreement 6%
70. Research Programmes 6%
71. External Pressure 6%
72. Static Pressure Distribution 6%
73. Aerodynamic Performance 6%
74. Pressure Distribution 6%
75. Lifecycle 6%
76. Flow Visualization 6%
77. Interaction Effect 6%
78. Design Concept 6%
79. Axial Location 6%
80. Turbine Inlet Temperature 6%
81. Gas Turbine Engine 6%
82. High Pressure Ratio 6%
83. Engine Performance 6%
84. High Efficiency 6%
85. Compressed Air 6%
86. Internals 6%
87. Air System 6%
88. Siemens 6%
89. Reduction 6%
90. Test Facility 6%
91. Fuel Cost 6%
92. Blade Profile 6%
93. Jet Propulsion 6%
94. Rotor Disc 6%
95. Fillet Geometry 6%
96. Planar Laser-Induced Fluorescence 6%
97. Turbine Components 6%
98. Cavity Flow 6%
99. Product 6%
100. Operating Cost 6%
101. Vortex Filament 5%
102. Supplied Air 5%