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All articles by "Selivanov A.N."
Constructing a turbine blade damage accumulation model for accounting the long-term operating time
| Authors: Sapronov D.V., Khudyakova A.D., Semenov A.V., Kosovsky D.V., Selivanov A.N. | Published: 16.11.2024 |
| Published in issue: #11(776)/2024 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: damage accumulation model, turbine blade service life, operating time, long-term strength, material creep |
Modeling of Residual Stresses when Calculating the Strength of Lock Joint Elements. Part 2. The Effect of Residual Stresses on the Stress-Strain State of the Turbine Blade Root
| Authors: Vasilyev B.E., Kiselev I.A., Zhukov N.A., Selivanov A.N. | Published: 24.12.2018 |
| Published in issue: #12(705)/2018 | |
| Category: Energy and Electrical Engineering | Chapter: Turbomachines and Combination Turbine Plants | |
| Keywords: residual stresses, shot peening, lock joint, turbine blade root, stress-strain state |
Modeling of Residual Stresses when Calculating Strength of Lock Joint Elements. Part 1. Modeling of the Shot Peening Process
| Authors: Kiselev I.A., Zhukov N.A., Vasilyev B.E., Selivanov A.N. | Published: 03.12.2018 |
| Published in issue: #11(704)/2018 | |
| Category: Energy and Electrical Engineering | Chapter: Turbomachines and Combination Turbine Plants | |
| Keywords: residual stresses, shot peening, finite element method, stress-strain state |