王 治武

Engineering

1. Afterburner 13%
2. Air Inlet 8%
3. Air Mixture 28%
4. Backpressure 26%
5. Breathing 49%
6. Bypass Ratio 8%
7. Combustion Chamber 7%
8. Combustor 13%
9. Computational Fluid Dynamics 6%
10. Convergent 8%
11. Deflagration 30%
12. Detonation Wave 34%
13. Duct 5%
14. Ejector 9%
15. Elastic Wave 23%
16. Equivalence Ratio 7%
17. Experimental Investigation 27%
18. Experimental Result 9%
19. Flight Altitude 5%
20. Flow Characteristic 10%
21. Flow Distribution 14%
22. Frequency Operation 7%
23. Hot Gas 6%
24. Ignition 18%
25. Initial Condition 9%
26. Initial Pressure 9%
27. Initiation Time 11%
28. Intake System 13%
29. Mixing Chamber 7%
30. Mockups 6%
31. Numerical Study 42%
32. Operating Characteristic 9%
33. Operating Frequency 16%
34. Oxidizer 5%
35. Partial Differential Equation 18%
36. Peak Pressure 12%
37. Physical Model 6%
38. Plenum Chamber 7%
39. Propagation Characteristic 5%
40. Pulse Detonation Engine 100%
41. Ratio Effect 5%
42. Simulation Result 16%
43. Stabilizer 7%
44. Transition to Detonation 28%
45. Turbine 32%
46. Two Dimensional 5%