张 文强

Engineering

1. Circumferential 100%
2. Rotors 65%
3. Computer Simulation 40%
4. Axial Compressors 37%
5. Duct 35%
6. Casing Treatment 32%
7. Feedback Control System 32%
8. Stall Cell 32%
9. Recovery Process 32%
10. Boundary Layer 29%
11. Snow and Ice Removal 27%
12. Fan Blade 26%
13. Aerodynamic Stability 25%
14. Airfoil 24%
15. Rotor Blade 21%
16. Parametric Study 20%
17. Drag Coefficient 20%
18. Lift Coefficient 20%
19. NASA 19%
20. Aero-Engines 18%
21. Nozzle Exit 18%
22. Axial-Flow Compressors 18%
23. Aeroengine 18%
24. Dynamic Response 16%
25. Temperature Region 16%
26. Aerodynamic Force 16%
27. Heating Surface 16%
28. Layer Flow 16%
29. Operational Condition 16%
30. Flow Compressor 16%
31. Tensile Stress σ 16%
32. Body Force 16%
33. Radial Distribution 16%
34. Constant Value 16%
35. Hydrophilicity 16%
36. Smooth Surface 16%
37. Roughness Effect 16%
38. Phase Flow 16%
39. Phase Field 16%
40. Spherical Interface 16%
41. Field Model 16%
42. Microstructure 16%
43. Penetration Depth 16%
44. Contact Time 16%
45. Numerical Study 16%
46. Pressure Ratio 16%
47. Vortex 15%
48. Rotating Stall 15%
49. Leading Edge 14%
50. Computational Fluid Dynamics 14%