Numerical Study of Influence of Inclined Crack Geometrical Characteristics in a Turbine Blade of the R-2617a Profile on a Failure Pressure in the Damage Detection System-Reference-Cited by-同舟云学术

Numerical Study of Influence of Inclined Crack Geometrical Characteristics in a Turbine Blade of the R-2617a Profile on a Failure Pressure in the Damage Detection System

Published:2024-03 Issue:1 Volume:67 Page:203-208
ISSN:1068-7998
Container-title:Russian Aeronautics
language:en
Short-container-title:Russ. Aeronaut.

Author:

Andrianov I. K.,Grinkrug M. S.,Kara Bally M.

Publisher

Allerton Press

Link

https://link.springer.com/content/pdf/10.3103/S1068799824010240.pdf

Reference15 articles.

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5. Petukhov, A.N. and Kiselev, F.D., Diagnostics of Operational Failures of Turbine Blades of Aircraft Engines, Zavodskaya Laboratoriya. Diagnostika Materialov, 2019, vol. 85, no. 3, pp. 41–51.