伊 卫林

Engineering

1. Design Optimization 100%
2. Aerodynamic Performance 89%
3. Rotors 78%
4. Compressor Blades 74%
5. Flow Field 72%
6. Numerical Study 71%
7. Centrifugal Compressor 71%
8. Optimization Method 70%
9. Turbomachinery 70%
10. Axial Compressors 60%
11. Flow Separation 59%
12. Impeller 59%
13. Streamwise 57%
14. Redesign 55%
15. Boundary Layer 53%
16. Pressure Ratio 46%
17. Blade Row 44%
18. Flow Structure 44%
19. Aerodynamic Design 43%
20. Diffusers 42%
21. Multistage 40%
22. High Pressure Ratio 40%
23. Response Surface 40%
24. Surface Model 40%
25. Centrifugal Impeller 39%
26. Suction Side 34%
27. Incidence Angle 34%
28. Computational Fluid Dynamics 33%
29. Dihedral Angle 33%
30. Genetic Algorithm 33%
31. NASA 31%
32. Numerical Optimization 31%
33. Leading Edge 30%
34. Secondary Flow 29%
35. Static Pressure Distribution 29%
36. Static Pressure 29%
37. Flow Mechanism 28%
38. Design Method 28%
39. Flow Distribution 28%
40. Experimental Result 26%
41. Circumferential 25%
42. Aerodynamics 24%
43. Computer Simulation 22%
44. Design Point 22%
45. Pressure Loss Coefficient 22%
46. Suction Surface 22%
47. Performance Improvement 21%
48. Volute 20%
49. Maximization 20%
50. Experimental Investigation 20%