Simulation of dynamic impact of an aircraft engine on aircraft wing caused by a fan blade breakaway
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Certification Specifications and Acceptable Means of Compliance for Large Aeroplanes CS-25. Amendment 14. 19 December 2013. 919 p. Available at: https://www.easa.europa.eu/sites/default/files/dfu/CS-25%20Amendment%2014.pdf. (accessed 10.03.2021).
Trekhval'nyi TRDD D-436-148. Rukovodstvo po tekhnicheskoi ekspluatatsii [Three-shaft turbofan engine D-436-148. Technical Manual] 6370040000 RE (In three books)., Zaporozh'e, «Ivchenko-Progress» Publ., 2008, Book 1. 1004 p.
Leont'ev, M. K. Konstrukcija i raschet dempfernyh opor rotorov GTD [Design and calculation of damping supports for GTE rotors]. Moscow, MAI Publ., 1998. 44 p.
Chigrin, V. S. Konstruktsiya i prochnost' aviatsionnykh dvigatelei [Design and strength of aircraft engines]. Khar'kov, Nat. Aerospace Univ. «KhAI», Zaporozh'e, «Motor Sich» Publ., 2017. 420 p.
Garkusha, A. I., Chigrin, V. S. Dinamika i prochnost' detalej gazoturbinnyh dvigatelej [Dynamics and strength of gas turbine engine parts]. Khar'kov, Nat. Aerospace Univ. «KhAI» Publ., 2012. 131 p.
Hronin, D. V. Teorija i raschet kolebanij v dvigateljah letatel'nyh apparatov [Theory and calculation of oscillation of aircraft engines]. Moscow, Mashinostroenie Publ, 1970. 412 p.
V'junov, S. A. Konstrukcija i proektirovanie aviacionnyh gazoturbinnyh dvigatelej [Design and engineering of aircraft gas turbine engines]. Moscow, Mashinostroenie Publ, 1989. 368 p.
DOI: https://doi.org/10.32620/aktt.2021.4sup1.10