动力与能源学院

Engineering

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