伊 卫林

Engineering

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