Author:
Bakulin V. N.,Nedbai A. Ya.
Publisher
Springer Science and Business Media LLC
Reference41 articles.
1. V. N. Bakulin, “Three-layer shells — effective elements of modern aircraft structures and strength analysis models, Proc. 14th Int. Conf. on Applied Math. and Mech. in the AerospaceI ndustry, MAI, Moscow, 270-272 (2022).
2. V. N. Bakulin, “Layer-by-layer study of the stress and strain state of sandwich conical aircraft compartments with rectangular cutouts,” Russian Aeronautics, 65, No. 4, 668-676 (2022).
3. V. N. Bakulin, “Investigation of the influence of the cutout dimensions on the stress-strain state of sandwich shells with load-carrying layers of composite materials,” J. Physics: Conf. Series: Mater. Sci. and Eng., 714, 012002 (2020).
4. A. V. Lopatin and A. A. Khakhlenkova, “Finite element modeling of a mesh composite coupling section of spacecraft,” Izv. RAN, Mekh. Tverd. Tela, 53, No. 4, 94-99 (2018).
5. N. A. Testoedov, V. N. Nagovitsin, and M. Yu. Permyakov, “The use of sandwich honeycomb structures in spacecraft,” Vestnik SibGAU, 17, No. 1, 200-211 (2016).