肖 旦丹

Engineering

1. Boundary Layer 100%
2. Airfoil 85%
3. Flow Field 64%
4. Layer Flow 57%
5. Direct Numerical Simulation 57%
6. Computer Simulation 57%
7. Flat Plate 53%
8. Drag Coefficient 53%
9. Lift Coefficient 53%
10. Leading Edge 50%
11. Secondary Instability 42%
12. Streamwise Vorticity 42%
13. Tensile Stress σ 42%
14. Streamwise 42%
15. Aerodynamic Force 42%
16. Field Data 42%
17. Optimal Control 42%
18. Heating Surface 42%
19. Constant Value 28%
20. Critical Reynolds Number 28%
21. Skin-Friction Coefficient 28%
22. Hydrophilicity 28%
23. Energy Flow 28%
24. Vorticity 24%
25. Angle-of-Attack 24%
26. Non-Linear Dynamic 21%
27. Plasma Fluid Model 21%
28. Flight Condition 21%
29. Separation Point 21%
30. Local Region 21%
31. Aerodynamic Drag 21%
32. Raw Data 21%
33. Aviation 21%
34. Activation Function 21%
35. Data Field 21%
36. Aerodynamic Coefficient 21%
37. Fourier Space 21%
38. Large Eddy Simulation 21%
39. Heating Temperature 21%
40. Flight Safety 21%
41. Light Detection and Ranging 21%
42. Simulation Result 21%
43. Gaussians 21%
44. Fluid Mechanics 21%
45. Accurate Prediction 21%
46. Numerical Data 21%
47. Reynolds-Averaged Navier-Stokes 21%
48. Nonlinear Response 21%
49. Threshold Temperature 14%
50. Nearest Neighbor 14%