School of Power and Energy

Engineering

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