Yong Xu

Engineering

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