伊 卫林

Engineering

1. Aerodynamic Performance 100%
2. Flow Field 85%
3. Numerical Study 84%
4. Centrifugal Compressor 76%
5. Streamwise 67%
6. Flow Separation 66%
7. Turbomachinery 63%
8. Boundary Layer 58%
9. Impeller 54%
10. Rotors 52%
11. Optimization Method 51%
12. Diffusers 50%
13. Compressor Blades 47%
14. Multistage 47%
15. Blade Row 47%
16. Axial Compressors 47%
17. High Pressure Ratio 47%
18. Centrifugal Impeller 46%
19. Redesign 41%
20. Suction Side 41%
21. Incidence Angle 41%
22. Design Optimization 41%
23. Computational Fluid Dynamics 39%
24. Dihedral Angle 39%
25. Pressure Ratio 39%
26. Flow Structure 36%
27. Secondary Flow 35%
28. Static Pressure Distribution 34%
29. Static Pressure 34%
30. Flow Mechanism 33%
31. Experimental Result 31%
32. Computer Simulation 26%
33. Design Point 26%
34. Pressure Loss Coefficient 26%
35. Suction Surface 26%
36. Performance Improvement 25%
37. Volute 23%
38. Maximization 23%
39. Genetic Algorithm 23%
40. Experimental Investigation 23%
41. Centrifugal Compressor Stage 23%
42. Circumferential 21%
43. Leading Edge 19%
44. Aerodynamic Shape Optimization 19%
45. Airfoil 19%
46. Aerodynamic Design 19%
47. Optimal Design 19%
48. Pressure Difference 18%
49. Mode Dynamic 18%
50. Stall Cell 18%