References
- 1. Gasparjans, A., Terebkovs, A., & Ziravecka, A. (2017). Application of resonance method for examining of piston ring technical condition. In 16th International Scientific Conference (pp. 884–891), 24–26 May 2017, Jelgava, Latvia (Elsevier SCOPUS, Thomson Reuters Web of Science, AGRIS, EBSCO Academic Search Complete, Agricola).10.22616/ERDev2017.16.N180
- 2. Gasparjans, A., Terebkovs, A., & Ziravecka, A. (2019). Theoretical and experimental analysis of technical condition of piston rings of vessel diesel installations by method of resonance oscillations. In 18th International Scientific Conference (pp. 1287–1294), 22–24 May 2019, Latvia University of Agriculture Faculty of Rural Engineering, Jelgava, Latvia. doi: 10.22616/ERDev2019.18.10.22616/ERDev2019.18
- 3. Pastorcic, D., Vukelic, G., & Bozic, Z. (2019). Coil Spring Failure and Fatigue Analysis. Eng. Fail. Anal., 1 (99), 310–318.10.1016/j.engfailanal.2019.02.017
- 4. Lukacs, J. (2019). Fatigue Crack Propagation Limit Curves for High Strength Steels Based on Two-Stage Relationship. Engineering Failure Analysis, 431–442.10.1016/j.engfailanal.2019.05.012
- 5. Cui, W. A (2002). State-of-the-Art Review on Fatigue Life Prediction Methods for Metal Structures. Journal of Marine Science and Technology, 7 (1), 43–56.10.1007/s007730200012
- 6. Schijve, J. (1979). Four Lectures on Fatigue Crack Growth. Engineering Fracture Mechanics, 169–181. doi:10.1016/0013-7944(79)90039-0. ISSN 0013-7944.10.1016/0013-7944(79)90039-0
- 7. Shaniavsky, A. A. (2003). Safe fatigue failure of aircraft structural elements. Ufa: Publishing house of scientific and technical literature “Monograph”.
- 8. Stoyda, Yu.M. (1988). The Development of the Method of Quantitative Fractography and the Study of Cyclic Crack Resistance of Structural Elements from Aluminium Alloys. The Doctoral Thesis. Moscow: VIAM.
- 9. Guide for Designers (RDK). (1980). Aircraft Strength (vol. 3), Fatigue Strength, Resource and Reliability of an Aircraft (book 4), Determination by the Method of Fractography of the Growth Duration of Fatigue Cracks in the Structural Elements of an Airframe (issue 12). M. Ed. Department of TsAGI.
- 10. Urbahs, A., & Carjova, K. (2018) Research on the Bolting Elements of Helicopter Fuselage and Tail Boom Joints Using Acoustic Emission Amplitude and Absolute Energy Criterion. American Journal of Aerospace Engineering, 32 (3). https://doi.org/10.1061/(ASCE)AS.1943-5525.000096310.1061/(ASCE)AS.1943-5525.0000963
- 11. Vizentin, G. (n.d.). Marine Propulsion System Failures – A Review. Available at https://www.mdpi.com/2077-1312/8/9/662/htm10.3390/jmse8090662
- 12. MAN Service Letter SL08-500/JNN, MAN Diesel
- 13. MAN Service Letter SL2018-656/JNN, MAN Diesel
- 14. MAN Diesel & Turbo. (2015). PrimeServ Customer Information No. 348/June 2015. Available at https://primeserv.man-es.com/docs/librariesprovider5/service-letter-marine/pci-348.pdf?sfvrsn=1cdb3fa2_4