李 军伟

Engineering

1. Rocket Engine 100%
2. Combustor 54%
3. Heptane 38%
4. Computer Simulation 36%
5. Flow Rate 32%
6. Microtube 28%
7. Combustion Chamber 23%
8. Oscillation Characteristic 22%
9. Highway Systems 20%
10. Equivalence Ratio 20%
11. Numerical Study 17%
12. Flame Stability 17%
13. Vortex Shedding 16%
14. Internals 15%
15. Mesoscale 15%
16. Chamber Pressure 14%
17. Couplings 13%
18. Damping Effect 13%
19. Transients 13%
20. Fuel Flow 13%
21. Heat Losses 12%
22. Gas Temperature 11%
23. Pressure Amplitude 10%
24. CH4 10%
25. Interior Ballistics 10%
26. Air Combustion 10%
27. Flow Field 10%
28. Rotary Valve 10%
29. Vortex 10%
30. Oxyfuel Combustion 10%
31. Diffusion Flame 10%
32. Evaporation Rate 9%
33. Mole Fraction 9%
34. Experimental Result 9%
35. Thermal Performance 9%
36. Cold Flow 9%
37. Energy Engineering 9%
38. Flame Temperature 8%
39. Microscale 8%
40. Burning Rate 8%
41. Resonance Damping 8%
42. Navier-Stokes Equation 8%
43. Aluminum Powder 8%
44. Experimental Investigation 7%
45. Air Velocity 7%
46. Ignition 7%
47. N-Heptane 7%
48. Burning Surface 7%
49. Oscillatory 7%
50. Two Dimensional 7%