School of Power and Energy

Engineering

1. Rotors 100%
2. Flow Distribution 85%
3. Turbine 79%
4. Experimental Investigation 70%
5. Vortex 65%
6. Aero-Engines 54%
7. Axial-Flow Compressors 53%
8. Leading Edge 53%
9. Casing Treatment 53%
10. Axial Compressors 51%
11. Pulse Detonation Engine 42%
12. Heat Transfer Coefficient 41%
13. Aerodynamic Performance 41%
14. Cooling Performance 39%
15. Pressure Ratio 38%
16. Leakage Flow 37%
17. Reynolds' Number 35%
18. Blade Tip 34%
19. Combustor 34%
20. Transients 32%
21. Suction Surface 32%
22. Numerical Study 32%
23. Blade Turbine 31%
24. Compressor Rotor 30%
25. Flow Characteristic 29%
26. Aeroengine 29%
27. Aerodynamics 27%
28. Secondary Flow 26%
29. Rocket Engine 26%
30. Detonation Wave 26%
31. Experimental Result 25%
32. Circumferential 24%
33. Trailing Edge 20%
34. Design Optimization 20%
35. Turbofan Engine 20%
36. Flow Velocity 19%
37. Simulation Result 19%
38. Ignition 19%
39. Compressor Performance 19%
40. Flow Mechanism 18%
41. Guide Vane 18%
42. Axisymmetric 18%
43. Boundary Layer 18%
44. Unsteady Flow 18%
45. Cooling Hole 18%
46. Flow Rate 18%
47. Engine Performance 18%
48. Deflagration 17%
49. Discharge Coefficient 17%
50. Pressure Loss 17%
51. Boundary Layer Suction 17%
52. Control System 17%
53. Computational Fluid Dynamics 17%
54. Rotor System 17%
55. Flow Separation 17%
56. Design Method 16%
57. Engine Cycle 16%
58. Suction Side 15%
59. Flow Structure 15%
60. Mass Flowrate 15%
61. Liquid Crystal 15%
62. Failure Probability 14%
63. Pressure Sensitive Paint 14%
64. Pressure Side 14%
65. Transition to Detonation 14%
66. Mach Number 14%
67. Pressure Surface 14%
68. Compressor Blade 14%
69. Turbulence Intensity 13%
70. Oxidizer 13%
71. Fault Diagnosis 13%
72. Design Point 13%
73. Convergent 13%
74. Impeller 13%
75. Incidence Angle 13%
76. Tunnel 12%
77. Temperature Distribution 12%
78. Blade Surface 12%
79. Numerical Method 12%
80. Rotor Blade 12%
81. Duct 11%
82. Pressure Distribution 11%
83. Reliability Analysis 11%
84. Centrifugal Pump 11%
85. Rotating Speed 11%
86. Airfoil 11%
87. Air Flow 11%
88. Simulation Method 11%
89. Diffusers 11%
90. Main Flow 11%
91. Static Pressure 11%
92. Flow Loss 10%
93. Peak Efficiency 10%
94. Nusselt Number 10%
95. Optimization Method 10%
96. Equivalence Ratio 10%
97. Two Dimensional 10%
98. Aircraft Engine 10%
99. Breathing 9%
100. Operating Frequency 9%