Dr Ashish Vashishtha

Engineering

1. Mach Number 100%
2. Numerical Study 66%
3. Computational Fluid Dynamics 61%
4. Hypersonic Flows 59%
5. Drag Reduction 56%
6. Convergent 54%
7. Flow Distribution 49%
8. Primary Jet 46%
9. Axisymmetric 42%
10. Bow Shock 40%
11. Flow in Nozzles 39%
12. Detonation Wave 39%
13. Mass Flowrate 28%
14. Experimental Result 26%
15. Duct 26%
16. Breathing 26%
17. Unsteady Flow 26%
18. Circular Nozzle 26%
19. Corner Radius 19%
20. Flow Investigation 19%
21. Gas Injection 19%
22. Orifice 19%
23. Base Pressure 19%
24. Vortex Flow 19%
25. Vortex 19%
26. Additive Manufacturing 19%
27. Direct Simulation 19%
28. Detached Eddy Simulation 19%
29. Flow Physic 19%
30. Building Interior 19%
31. One Dimensional 19%
32. Vortex Generator 19%
33. Thick Airfoil 19%
34. Compressed Air Motors 19%
35. Impact Pressure 19%
36. Droplet Size 19%
37. Two Dimensional 18%
38. Axial Distance 16%
39. Nozzle Exit 16%
40. Boundary Condition 14%
41. Pressure Distribution 14%
42. Ignition 14%
43. Hypersonic Speed 14%
44. Primary Nozzle 13%
45. Re-Entry Vehicle 13%
46. Collection Efficiency 13%
47. Electric Propulsion 13%
48. Operational Life 13%
49. Combustion Zone 13%
50. Gas-Phase 13%