刘 存良

Engineering

1. Cooling Performance 100%
2. Heat Transfer Coefficient 74%
3. Turbine 70%
4. Leading Edge 45%
5. Blade Turbine 43%
6. Experimental Investigation 37%
7. Reynolds' Number 34%
8. Transients 30%
9. Vortex 29%
10. Turbulence Intensity 25%
11. Discharge Coefficient 25%
12. Numerical Study 22%
13. Liquid Crystal 22%
14. Pressure Sensitive Paint 21%
15. Flow Structure 17%
16. Suction Surface 17%
17. Cooling Hole 16%
18. Nusselt Number 16%
19. Density Ratio 16%
20. Pressure Side 16%
21. Flow Distribution 15%
22. Trailing Edge 15%
23. Heat Flux 15%
24. Superposition 14%
25. Suction Side 14%
26. Double Wall 14%
27. Pressure Surface 13%
28. Leakage Flow 12%
29. Momentum Flux 12%
30. Secondary Flow 11%
31. Flow Characteristic 11%
32. Coolant Flow 11%
33. Thermal Conductivity 11%
34. Gas Turbine 10%
35. Cooling Scheme 10%
36. Blade Tip 10%
37. Inclination Angle 9%
38. Cooling System 9%
39. Heat Shield 9%
40. Duct 9%
41. Flat Plate 9%
42. Thermochromic Liquid Crystal 8%
43. Target Plate 8%
44. Aerodynamics 8%
45. Area Ratio 8%
46. Pressure Gradient 8%
47. Jet Reynolds Number 8%
48. Resistance Characteristic 8%
49. Cooling Air 7%
50. Experimental Result 7%