An investigation into combined film and internal cooling of turbine blades

Engineering

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