ESTIMATION OF THE STRESS-STRAIN STATE OF A GAS TURBINE ENGINE BLADES by LASER OPTICAL-ACOUSTIC METHOD
Possibility of the use of the laser generation of surface acoustic waves in the blades of aircraft gas turbine engines, registration, processing and analysis of the acoustic waves parameters to assess the possibility of determination of residual stresses is considered.
| Main Authors: | , , , |
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| Format: | Article |
| Language: | Russian |
| Published: |
Moscow State Technical University of Civil Aviation
2016-11-01
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| Series: | Научный вестник МГТУ ГА |
| Subjects: | |
| Online Access: | https://avia.mstuca.ru/jour/article/view/217 |