Modeling of Interaction of the Mechatronic Unit Segments in the Adaptable Part of an Aircraft Wing

Author:

Sharonov N.,Makarov A.,Ivchenko A.,Gorelova A.

Publisher

Springer International Publishing

Reference20 articles.

1. Ivchenko, A.V., Sharonov, N.D.: The mechatronic unit and frame adaptable wing. Prog. Veh. Syst. 176–177 (2018)

2. Barbarino, S., Bilgeno, O., Ajaj, R.M., et al.: A review of morphing aircraft. J. Intell. Mater. Syst. Struct. 22, 823–877 (2011)

3. Monner, H.P., Bein, T., Hanselka, H., et al.: Design aspect of the adaptive wing – the elastic trailing edge and the local spoiler bump. In: Proceeding of Royal Aeronautical Society Symposium on Multidisciplinary Design and Optimization, pp. 15.1–15.9. Royal Society Publishing (1998)

4. Pecora, R., Barbarino, S., Concilio, A., et al.: Design and functional test of a morphing high-lift device for a regional aircraft. J. Intell. Mater. Syst. Struct. 22(10), 1005–1023 (2011)

5. Pecora, R., Amoroso, F., Lecce, L.: Effectiveness of wing twist morphing in roll control. J. Aircr. 49(6), 1666–1674 (2012)

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