刘 波

Engineering

1. Rotors 100%
2. Flow Distribution 79%
3. Vortex 66%
4. Axial Compressors 61%
5. Leakage Flow 58%
6. Boundary Layer Suction 56%
7. Suction Surface 52%
8. Axial-Flow Compressors 41%
9. Design Optimization 38%
10. Incidence Angle 35%
11. Aerodynamic Performance 34%
12. Axisymmetric 33%
13. Pressure Ratio 33%
14. Flow Separation 31%
15. Boundary Layer 31%
16. Trailing Edge 31%
17. Airfoil 25%
18. Leading Edge 24%
19. Multistage 23%
20. Pressure Loss 21%
21. Static Pressure 19%
22. Secondary Flow 18%
23. Unsteady Flow 18%
24. Blade Tip 18%
25. Flow Velocity 18%
26. Flow Rate 18%
27. Design Point 18%
28. Flow Structure 16%
29. Loss Coefficient 16%
30. Guide Vane 16%
31. Separation Control 16%
32. Compressor Blade 14%
33. Compressor Performance 14%
34. Pressure Loss Coefficient 13%
35. Circumferential 13%
36. Design Condition 13%
37. Boundary Layer Separation 13%
38. Peak Efficiency 12%
39. Casing Treatment 12%
40. Rotating Stall 12%
41. Turbine 12%
42. Isentropic Efficiency 11%
43. Angle of Incidence 11%
44. Compressor Rotor 11%
45. Tunnel 11%
46. Flow Mechanism 11%
47. Main Flow 10%
48. Rotor Blade 10%
49. Pressure Distribution 10%
50. Rotating Speed 10%