1. V. V. Ovchinnicov and Yu. V. Petrov, Numerical Methods for the Study of Aircraft Aeroelasticity (Izdat. Dom Acad. Zhukovskogo, Moscow, 2017) [in Russian].
2. W. P. Rodden, Theoretical and Computational Aeroelasticity (Crest Publishing, 2011).
3. S. Waitz and H. Hennings, “The aeroelastic impact of engine thrust and gyroscopics on aircraft flutter instabilities,” in 16th International Forum on Aeroelasticity and Structural Dynamics (IFASD-2015), June 28–July 02,
2015, St. Petersburg, Russia (St. Petersburg, 2015), pp. 1–15.
4. M. Fujino, H. Oyama, and H. Omotani, “Flutter characteristics of an over-the-wing engine mount business-jet configuration,” in 44th AiAA/ASME/ASCE/AHS Structures, Structural Dynamics and Materials Conference 8-10 April
2003, Norfolk, Virginia (AIAA 2003–1942), pp. 1–12. https://doi.org/10.2514/6.2003-1942
5. L. Wang, Zh. Wan, Q. Wu, and C. Yang, “Aeroelastic modeling and analysis of the wing / engine system of a large aircraft,” Procedia Eng. 31, 879–885, (2012). https://doi.org/10.1016/j.proeng.2012.01.1116