AERONAUTICAL AND MECHANICAL PROJECTS | COLLEGE STUDENTS LIVE
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AERONAUTICAL AND MECHANICAL PROJECTS


1. Aero spike nozzle analysis
2. Design and analysis of oblique flying wing
3. Design and analysis of hover bike
4. Design and analysis of liquid propellant rocket engine
5. Design and analysis of subsonic blended body aircraft
6. Design and analysis of super critical aero foil in transonic region
7. Design and analysis of turbojet engine for reducing noX
8. Design and analysis ofUAV
9. Flutter analysis in delta wing with stores
10. High speed aspect ratio wing in ground effect
11. Modification and analysis of pulse jet engine
12. Study of variation of drag over
13. Thermal fatigue analysis of turbine blade
14. Vortex interaction and breakdown over cranked arrow wing
15. Aerodynamic analysis of sports sedan
16. Aerodynamic analysis of low speed performance of simple and compound delta wing
17. Computational analysis of low pressure turbine blade
18. Conceptual design and analysis of aerospace nozzle
19. Design and analysis of 2d inlet for air augmented missile
20. Design and analysis of personal air vehicle
21. Design and analysis of supersonic combustor with ramp- cavity fuel injector
22. Design and analysis of cave wing
23. Design and analysis of hypersonic inlets
24. Design and study of hybrid UAV
25. Drag reduction of bluff body at hypersonic speed
26. Drag reduction studies on blunt body by using spike devices
27. Eddy current retarder
28. Flame stabilization in scramjet combustor
29. Micro unmanned aerial vehicle design-towards long endurance
30. Stress analysis in various types of fly wheels
31. Structural analysis of wing lug
32. Structural analysis of wing bracket
33. Fatigue and structural analysis of wing lug
34. Stress analysis and fatigue life evaluation for a wing-fuselage lug attachment bracket of a transport aircraft
35. Comparison of structural analysis of delta wing using composite materials
36. Ramjet combustion flame stabilization using air curtains from perforated wall
37. Gust analysis of different wing system
38. Reduction of turbine induced turbulence using riblets
39. Optimizing the combustion efficiency of ramjet engine using bluff body flame stabilizer

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