张 皓光

Engineering

1. Casing Treatment 100%
2. Axial-Flow Compressors 62%
3. Axial Compressors 60%
4. Rotors 53%
5. Vortex 45%
6. Blade Tip 37%
7. Flow Distribution 37%
8. Compressor Rotor 36%
9. Circumferential 30%
10. Compressor Performance 27%
11. Flow Mechanism 24%
12. Leading Edge 23%
13. Leakage Flow 23%
14. Secondary Flow 15%
15. Blade Angle 15%
16. Aerodynamic Performance 14%
17. Aerodynamics 14%
18. Flow Loss 12%
19. Vortex Generator 11%
20. Peak Efficiency 11%
21. Unsteady Flow 8%
22. Boundary Layer Separation 8%
23. Suction Surface 7%
24. Pressure Ratio 6%
25. Numerical Study 6%
26. Design Point 6%
27. Stability Margin 6%
28. Compressor Efficiency 6%
29. Flow Condition 6%
30. NASA 6%
31. Boundary Layer Suction 6%
32. Mass Flowrate 6%
33. Rotating Speed 6%
34. Operating Range 6%
35. Blade Surface 5%
36. Boundary Layer 5%
37. Blade Passage 5%
38. Impeller 5%
39. Axisymmetric 5%
40. Centrifugal Fan 5%
41. Efficiency Loss 5%
42. Volute 5%
43. Numerical Method 5%
44. Pressure Loss 5%
45. Peak Velocity 5%
46. Uncertainty Quantification 5%