方 蜀州

Engineering

1. Drag Reduction 100%
2. Hypersonic Vehicles 90%
3. Thruster 81%
4. Blunt Body 68%
5. Heat Flux 68%
6. Computer Simulation 66%
7. Ignition 63%
8. Aerodynamic Performance 56%
9. Thermal Protection 55%
10. Combustion Chamber 42%
11. Flow Field 41%
12. Attitude Control 38%
13. Drag Coefficient 37%
14. Space Vehicle 34%
15. Numerical Study 32%
16. Angle-of-Attack 32%
17. Performance Analysis 30%
18. Two Dimensional 30%
19. Leading Edge 30%
20. Direct Simulation 28%
21. Orbit Control 28%
22. Coupled Circuits 27%
23. Hypersonic Flows 27%
24. Stanton Number 24%
25. Mach Number 23%
26. Micro Turbine 23%
27. Simulation Result 23%
28. Stagnation Point 22%
29. Airfoil 20%
30. Turbojet Engine 20%
31. Interconnects 20%
32. Flow Characteristics 18%
33. Boundary Element Method 17%
34. Coordinate System 17%
35. Burning Surface 16%
36. Annular Combustor 15%
37. Combustor 15%
38. Lift Coefficient 14%
39. Boundary Condition 13%
40. Heat Losses 13%
41. Thermal Radiation 13%
42. Simulation Method 13%
43. Drag Ratio 13%
44. Aerothermal Performance 11%
45. Turbine 10%
46. Characteristic Vibration 10%
47. Extractor 10%
48. Rocket Engine 10%
49. Annular Combustion Chamber 10%
50. Solenoid Valve 10%