伊 卫林

Engineering

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