刘 艳明

Engineering

1. Vortex 100%
2. Computer Simulation 79%
3. Secondary Flow 65%
4. Flow Field 51%
5. Synthetic Jet Actuator 49%
6. Centrifugal Compressor 49%
7. Leading Edge 40%
8. Boundary Layer 33%
9. Gas Turbine 33%
10. Aerodynamic Performance 31%
11. Axial Compressors 24%
12. Pressure Side 24%
13. Streamwise 21%
14. Diffusers 20%
15. Pressure Ratio 19%
16. Primary Jet 18%
17. Pressure Loss 18%
18. Pressure Surface 17%
19. Compressor Performance 16%
20. Intake System 16%
21. Separation Control 16%
22. Micro-Jet 16%
23. Aerodynamics 16%
24. Boundary Layer Thickness 16%
25. Control System 14%
26. Control Flow 14%
27. Actuation 13%
28. Suction Side 13%
29. Suction Surface 13%
30. Uncertainty Quantification 12%
31. Design Optimization 12%
32. Flow Mechanism 12%
33. Vortex Generator 11%
34. Mass Transfer 10%
35. Actuator Configuration 10%
36. Trailing Edge 10%
37. Field Performance 9%
38. Piston Displacement 9%
39. Rotating Speed 9%
40. Energy Dissipation 9%
41. Horseshoe Vortex 9%
42. Supersonic Flow 9%
43. Blade Tip 8%
44. Two Dimensional 8%
45. Static Pressure Coefficient 8%
46. Sweep Angle 8%
47. Exit Plane 8%
48. Numerical Modeling 8%
49. Performance Prediction 8%
50. Edge Effect 8%