徐 勇

Engineering

1. Drag Reduction 100%
2. Heat Flux 93%
3. Blunt Body 91%
4. Hypersonic Vehicles 80%
5. Aerodynamic Performance 70%
6. Flow Field 47%
7. Numerical Study 43%
8. Space Vehicle 39%
9. Drag Coefficient 36%
10. Thermal Protection 36%
11. Stanton Number 33%
12. Hypersonic Flows 33%
13. Computer Simulation 29%
14. Stagnation Point 23%
15. Angle-of-Attack 22%
16. Performance Analysis 19%
17. Aerothermodynamics 19%
18. Aerodynamic Analysis 19%
19. Airfoil 19%
20. Leading Edge 19%
21. Model Combination 19%
22. Aerothermal Performance 17%
23. Reattachment 17%
24. Two Dimensional 16%
25. Axisymmetric 16%
26. Direct Simulation 16%
27. Thermal Load 14%
28. Aerodynamic Drag 14%
29. Lift to Drag Ratio 13%
30. Diameter Ratio 13%
31. Flow Characteristics 13%
32. Depth Ratio 13%
33. Change Rate 10%
34. Air Pressure 9%
35. Three-Dimensional Models 9%
36. Peak Value 9%
37. Cooling Performance 9%
38. Nozzle Exit 9%
39. Solid Spike 9%
40. Heat Flux Density 9%
41. Navier-Stokes Equation 9%
42. Channel Structure 9%
43. Major Problem 9%
44. High Pressure and High Temperature 9%
45. Reynolds-Averaged Navier-Stokes 9%
46. Asymmetric Flow 9%
47. Flow Phenomenon 9%
48. Dimensional Flow Field 9%
49. Aspect Ratio 9%
50. Diameter Channel 7%