Modelling of Buyancy-Induced Flow in Compressor Rotors - Surrey/RR

Engineering

1. Compressor Rotor 100%
2. Rotating Cavity 55%
3. Compressibility 51%
4. Radial Distribution 49%
5. Rotating Disk 47%
6. Grashof Number 44%
7. Heat Flux 43%
8. Temperature Distribution 42%
9. Nusselt Number 41%
10. Transients 41%
11. Closed Rotating Cavity 38%
12. Aero-Engines 37%
13. Throughflow 36%
14. Vortex 36%
15. Gas Turbine 31%
16. Engine Designer 28%
17. Flow Structure 27%
18. Pressure Ratio 27%
19. Rotating Flow 26%
20. Aeroengine 26%
21. Core Temperature 25%
22. Core Fluid 23%
23. Blade Tip 21%
24. Axial Throughflow 20%
25. Compressor Blades 19%
26. Rotational Speed 18%
27. Experimental Range 18%
28. Good Agreement 17%
29. Rotational Reynolds Number 17%
30. Convective 16%
31. Accurate Prediction 16%
32. Experimental Investigation 15%
33. Flow Phenomenon 15%
34. Bayesian Model 13%
35. Natural Convection 13%
36. Computational Fluid Dynamics 13%
37. Boundary Condition 12%
38. Aircraft Engine 12%
39. Engine Design 12%
40. Ekman Layer 11%
41. Two Dimensional 11%
42. One Dimensional 11%
43. Reynolds' Number 11%
44. Temperature Rise 11%
45. Buoyancy Effect 11%
46. Rossby Number 10%
47. Collected Data 10%
48. Pressure Sensor 10%
49. Rotating Fluid 10%
50. Unsteady Flow 10%
51. Industrial Gas Turbine 9%
52. Thermocouple 9%
53. Radial Clearance 9%
54. Forced Convection 9%
55. Cold Fluid 9%
56. Hot Fluid 9%
57. Mainstream Flow 8%
58. Cooling Air 8%
59. Fluid Dynamics 8%
60. Rotating Core 8%
61. Biot Number 7%
62. Thermopile 7%
63. Bayes Theorem 7%
64. Single Curve 7%
65. Heat Flux Gauge 7%
66. Temperature Increase 7%
67. Limitations 7%
68. Mass Flowrate 7%
69. Gas Turbine Engine 7%
70. Rotors 6%
71. Disc Surface 6%
72. Buoyancy Force 6%
73. Cavity 6%
74. Mixing Region 5%
75. Thermal Stress 5%
76. Layer Flow 5%
77. Fitting Curve 5%
78. Jet Engine 5%
79. Relative Error 5%
80. Flow Characteristics 5%
81. Radial Outflow 5%
82. Temperature Stress 5%
83. Thermal Gradient 5%
84. Mechanical Design 5%
85. Fluid Domain 5%
86. Pressure Difference 5%
87. Flow Configuration 5%
88. Thermal Inertia 5%
89. Circumferential 5%