Development of Reduced Order Strain Model for Life Assessment of a Gas Turbine Rotor Blade
Compressor rotor blades of Gas Turbine Engines are critical components in the flow path. Their durability is determined by Life and integrity at different operating conditions. These blades experience stresses due to body loads and complex bending stresse
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S. Seetharamu Thimmarayappa Jagadish Ravindra R. Malagi Editors
Fatigue, Durability, and Fracture Mechanics Proceedings of Fatigue Durability India 2019
Lecture Notes in Mechanical Engineering Series Editors Francisco Cavas-Martínez, Departamento de Estructuras, Universidad Politécnica de Cartagena, Cartagena, Murcia, Spain Fakher Chaari, National School of Engineers, University of Sfax, Sfax, Tunisia Francesco Gherardini, Dipartimento di Ingegneria, Università di Modena e Reggio Emilia, Modena, Italy Mohamed Haddar, National School of Engineers of Sfax (ENIS), Sfax, Tunisia Vitalii Ivanov, Department of Manufacturing Engineering Machine and Tools, Sumy State University, Sumy, Ukraine Young W. Kwon, Department of Manufacturing Engineering and Aerospace Engineering, Graduate School of Engineering and Applied Science, Monterey, CA, USA Justyna Trojanowska, Poznan University of Technology, Poznan, Poland
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S. Seetharamu Thimmarayappa Jagadish Ravindra R. Malagi •
•
Editors
Fatigue, Durability, and Fracture Mechanics Proceedings of Fatigue Durability India 2019
123
Editors S. Seetharamu Central Power Research Institute Bangalore, Karnataka, India
Thimmarayappa Jagadish DHIO Research and Engineering Pvt Ltd Bangalore, Karnataka, India
Ravindra R. Malagi Mechanical Department KLS Gogte Institute of Technology Belagavi, Karnataka, India
ISSN 2195-4356 ISSN 2195-4364 (electronic) Lecture Notes in Mechanical Engineering ISBN 97
