孙 士珺

Engineering

1. Aerodynamic Performance 100%
2. Rotors 85%
3. Pressure Ratio 79%
4. Boundary Layer Suction 58%
5. Leading Edge 57%
6. Flow Characteristics 56%
7. Aerodynamic Design 52%
8. Computer Simulation 51%
9. Boundary Layer 51%
10. Suction Surface 48%
11. Compressor Rotor 43%
12. Peak Efficiency 43%
13. Flow Separation 39%
14. Design Method 32%
15. Inlet Mach Number 31%
16. Throughflow 29%
17. Aerodynamic Analysis 29%
18. Compressor Stage 29%
19. Centrifugal Compressor 29%
20. Leakage Flow 26%
21. Vortex 26%
22. Trailing Edge 25%
23. Rotational Speed 25%
24. Secondary Flow 25%
25. Axial Compressors 25%
26. Flow Field 25%
27. Turbomachinery 24%
28. Flow Visualization 23%
29. Pressure Side 23%
30. Limiting Streamlines 21%
31. Gas Turbine 21%
32. Design Analysis 19%
33. Axial Velocity 19%
34. Flow Fraction 19%
35. Blade Tip 18%
36. Pressure Loss 18%
37. Mach Number 18%
38. Aerodynamics 18%
39. Numerical Study 18%
40. Operating Range 17%
41. Flow Structure 16%
42. Simulation Result 15%
43. Pressure Surface 14%
44. Boundary Layer Thickness 14%
45. Diffusers 14%
46. Optimised Design 14%
47. Experimental Investigation 14%
48. Performance Analysis 14%
49. Centrifugal Fan 14%
50. Sweep Angle 14%