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. Vortex 90%
3. Secondary Flow 86%
4. Flow Distribution 56%
5. Rotors 55%
6. Gas Turbine 43%
7. Flow Structure 40%
8. Horseshoe Vortex 39%
9. Pressure Side 35%
10. Jet 31%
11. Axisymmetric 30%
12. Mainstream Flow 28%
13. Blade Passage 27%
14. Suction Side 26%
15. Single Stage Turbine 26%
16. Computational Fluid Dynamics 23%
17. Momentum Flux 18%
18. Pressure Distribution 18%
19. Fluid Dynamics 17%
20. Turbomachinery 16%
21. Disc Turbine 15%
22. Turbine Efficiency 15%
23. Blade Row 15%
24. Borescope 15%
25. Measurement System 15%
26. Design Tool 15%
27. Leading Edge 14%
28. Static Pressure 13%
29. Cycle Efficiency 12%
30. Velocity Field 11%
31. Guide Vane 10%
32. Rotational 10%
33. Vortex Filament 9%
34. Test Rig 8%
35. Suction Surface 8%
36. Aerodynamics 8%
37. External Pressure 7%
38. Aerodynamic Performance 7%
39. Lifecycle 7%
40. Flow Visualization 7%
41. Design Concept 7%
42. Turbine Inlet Temperature 7%
43. Gas Turbine Engine 7%
44. High Pressure Ratio 7%
45. Engine Performance 7%
46. Air System 7%
47. Siemens 7%
48. Fuel Cost 7%
49. Blade Profile 7%
50. Rotor Disc 7%
51. Fillet Geometry 7%
52. Turbine Components 7%
53. Operating Cost 7%
54. Jet Propulsion 7%
55. Compressed Air 7%
56. Laser Beams 7%
57. Legislation 7%
58. Electric Power 7%
59. Flowrates 7%
60. Experimental Technique 6%
61. Induced Velocity 6%
62. Quality Data 6%
63. Main Flow 6%
64. Good Agreement 6%
65. Boundary Condition 6%
66. Particle Image Velocimetry 6%
67. Field Measurement 6%
68. Flow Condition 6%
69. Static Pressure Distribution 5%
70. Interaction Effect 5%
71. Axial Location 5%
72. Test Facility 5%
73. Planar Laser-Induced Fluorescence 5%
74. Cavity Flow 5%