Elastoplastic Thermo-mechanical Stressed State of Turbine Blades Locking Joints
Author:
Publisher
Springer International Publishing
Link
https://link.springer.com/content/pdf/10.1007/978-3-031-18487-1_22
Reference17 articles.
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4. Branda, P., Infante, V., Deus, A.M.: Thermo-mechanical modeling of a high pressure turbine blade of an airplane gas turbine engine. Procedia Struct. Integrity 1, 189–196 (2016)
5. Kumar, R., Kumar, V.S., Butt, M.M., Seikh, N.A., Khan, S.A., Afzal, A.: Thermo-mechanical analysis and estimation of turbine blade tip clearance of a small gas turbine engine under transient operating conditions. Appl. Therm. Eng. 179, 115700 (2020)
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