| 2026, 05 May |
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DOI: 10.14489/td.2026.05.pp.033-038 Popov A. V., Voloshina V. Yu., Lebedinsky M. S., Krivoshein D. S. Abstract. The article discusses a method for identifying defects in composite structures based on acoustic emission invariants, using the deviation of acoustic emission pulse number distribution parameters from a Poisson shape as a criterion for macrocrack formation. The results of experimental studies of samples making from organic glass used in the manufacture of pressurized aircraft cabin glazing are presented. Keywords: aircraft, cabin glazing, organic glass, macrocrack, fracture.
A. V. Popov, V. Yu. Voloshina, M. S. Lebedinsky (Military Educational and Scientific Center of the Air Force, N. E. Zhukovsky and Y. A. Gagarin Air Force Academy, Voronezh, Russia) E-mail:
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1. Sereznov, A. N., Stepanova, L. N., Kabanov, S. I., et al. (2008). Acoustic emission testing of aircraft structures (L. N. Stepanova & A. N. Sereznov, Eds.). Mashinostroe-nie – Polet. [in Russian language].
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