Hui Tang

Engineering

1. Compressor Rotor 100%
2. Rotating Disk 76%
3. Nusselt Number 73%
4. Radial Distribution 67%
5. Flow Structure 58%
6. Rotating Cavity 58%
7. Throughflow 56%
8. Grashof Number 53%
9. Aero-Engines 52%
10. Heat Flux 51%
11. Compressibility 44%
12. Transients 43%
13. Temperature Distribution 42%
14. Axial Throughflow 38%
15. Aeroengine 36%
16. Vortex 35%
17. Engine Designer 34%
18. Closed Rotating Cavity 32%
19. Pressure Ratio 30%
20. Core Temperature 27%
21. Blade Tip 26%
22. Rotors 25%
23. Hot Gas 25%
24. Gas Turbine 22%
25. Swirl Ratio 22%
26. Rotating Flow 21%
27. Good Agreement 21%
28. Rotational Speed 19%
29. Core Fluid 18%
30. Rossby Number 18%
31. Rotational Reynolds Number 18%
32. Natural Convection 18%
33. Ekman Layer 18%
34. Accurate Prediction 17%
35. Compressor Blades 17%
36. Convective 15%
37. Experimental Range 14%
38. Turbine 14%
39. Computational Fluid Dynamics 14%
40. Mass Exchange 14%
41. Boundary Condition 13%
42. Experimental Measurement 13%
43. Thermocouple 13%
44. Flow Physic 13%
45. Cooling Air 13%
46. Experimental Investigation 12%
47. Flow Phenomenon 12%
48. Heat Exchange 12%
49. Disc Turbine 12%
50. Thermal Gradient 12%