An investigation into combined film and internal cooling of turbine blades

Engineering

1. Performance 100%
2. Effect of Porosity 100%
3. Porosity 100%
4. Temperature 83%
5. Cooling Performance 66%
6. Blade Turbine 50%
7. Internals 50%
8. Surface 43%
9. Engine Efficiency 40%
10. Gas Turbine 40%
11. Design 40%
12. Polymers 33%
13. High Resolution 33%
14. Test Coupon 33%
15. Infrared Thermography 33%
16. Tunnels 33%
17. Experimental Measurement 33%
18. Small Scale 33%
19. Micron 33%
20. Models 30%
21. Fluid 30%
22. Measurement 20%
23. Heat Transfer 20%
24. Measurement System 20%
25. Test Piece 20%
26. Velocity Component 10%
27. Primary User 10%
28. Research 10%
29. Fluid Dynamics 10%
30. External Surface 10%
31. Fossil Fuel 10%
32. Turbine 10%
33. Redesign 10%
34. Blade Cooling 10%
35. Cooling Hole 10%
36. Melting Point 10%
37. Prediction 10%
38. Facilities 10%
39. Internal Surface 10%
40. Heat Transfer Coefficient 10%
41. Engine 10%
42. Stages 10%
43. Cooling Scheme 10%
44. Concentration Field 10%
45. Error 10%
46. Efficiency 10%
47. Siemens 10%
48. Product 10%
49. High Precision 10%
50. Alloy 10%
51. Thin Films 10%
52. Isentropic Efficiency 10%