Author:
Eshati S.,Abu A.,Laskaridis P.,Khan F.
Subject
Industrial and Manufacturing Engineering,Energy Engineering and Power Technology
Reference64 articles.
1. Rotor blade cooling in high pressure turbine;Holland;Journal of Aircraft,1980
2. A new method to calculate the coolant requirements of a high-temperature gas turbine blade;Torbidoni;Journal of Turbomachinary,2005
3. Implementation of creep-fatigue model into finite element code to assess cooled turbine blade;Dedekind;International Journal of Pressure Vessels and Piping,1994
4. Integrated Lifing Analysis Tool for Gas Turbine Components;Tinga,2000
5. V.G. Karaivanov, D.W. Mazzotta, M.K. Chyu, W.S. Slaughter, M.A. Alvin, Three-dimensional modeling of creep damage in airfoils for advanced turbine system, in: Proceeding of ASME Turbo Expo 2008: Power for Land, Sea and Air, 9–13, June, Berlin, Germany, 2008.
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