Hui Tang

Engineering

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