Material testing for fatigue design of heavy-duty gas turbine blading with film cooling

European Structural Integrity Society

Volumn 23, Issue C, 1999, Pages 155-162

  Pan, Ying ^a   Bischoff Beiermann, Burkhard ^a   Schulenberg, Thomas ^a  

^a SIEMENS AG   (Germany)

Author keywords

Heavy duty gas turbine, film cooling hole, low cycle fatigue, fatigue life, FE calculation

Indexed keywords

EID: 33748550599     PISSN: 15661369     EISSN: None     Source Type: Book Series    
DOI: 10.1016/S1566-1369(99)80038-7     Document Type: Article

References (6)

1. Becker B., Schulenberg T., and Termuehlen H. The 3A Series Gas Turbines with HBR Combustors. ASME 95-GT-456 (1995), Turbo Expo, Houston, Texas
2. Seeger T., and Heuler P. Generalised Application of Neuber's rule. J. Test. Eval. 3 (1980) 199-204
3. Savaidis G., Dankert M., and Seeger T. An Analytical Procedure for Predicting Opening Loads of Cracks at Notches. Fatigue Fract. Engng Mater. Struct. Vol. 18 No. 4 (1995) 425-442
4. Neuber H. Theroy of Stress Concentration for S hear-Strained Prismatical Bodies with Arbitrary Nonlinear Stress-Strain Law. Journal of Applied Mechanics 12 (1961) 544-550
5. Chaudonneret M., and Chaboche J.L. Fatigue Life Prediction of Notched Specimens. Int. Conf of Fatigue of Engineering Materials and Structures. Sheffield (1988)
6. Lemaitre J. A Course on Damage Mechanics (1992), Springer Verlag