刘 波

Engineering

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