Thermal Distribution on Gas Turbine Blade Using Thermal Paint
113
15. Dedekind MO, Harris LE (1996) Evaluation of premature failure of a gas turbine component.
Int J Press Vessel Pip 66(1–3):59–76
16. Chmielniak T, Lepszy S, Rulik S (2011) Algorithm for design calculation of axial flow
gas turbine compressor-comparison with GTD-350 compressor design. Mech Mech Eng
15(3):207–216
17. Bhalerao SV, Pawar AN (2012) Thermal analysis of an aero-gas turbine compressor blade and
vane using temperature sensing thermal paints. Int J Adv Sci Res Technol 2(2):286–292
18. Lee JJ, Dutton JC, Jacobi AM (2007) Application of temperature-sensitive paint for surface
temperature measurement in heat transfer enhancement applications. J Mech Sci Technol
21:1253–1262
113
15. Dedekind MO, Harris LE (1996) Evaluation of premature failure of a gas turbine component.
Int J Press Vessel Pip 66(1–3):59–76
16. Chmielniak T, Lepszy S, Rulik S (2011) Algorithm for design calculation of axial flow
gas turbine compressor-comparison with GTD-350 compressor design. Mech Mech Eng
15(3):207–216
17. Bhalerao SV, Pawar AN (2012) Thermal analysis of an aero-gas turbine compressor blade and
vane using temperature sensing thermal paints. Int J Adv Sci Res Technol 2(2):286–292
18. Lee JJ, Dutton JC, Jacobi AM (2007) Application of temperature-sensitive paint for surface
temperature measurement in heat transfer enhancement applications. J Mech Sci Technol
21:1253–1262