Three-Dimensional Stress-Strain State Analysis of the Bimetallic Launch Vehicle Propellant Tank Shell
Author:
Publisher
Springer Science and Business Media LLC
Subject
Mechanics of Materials
Link
https://link.springer.com/content/pdf/10.1007/s11223-023-00582-9.pdf
Reference24 articles.
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4. P. Gontarovskyi, N. Smetankina, N. Garmash, and I. Melezhyk, “Numerical analysis of stress-strain state of fuel tanks of launch vehicles in 3D formulation,” in: M. Nechyporuk, V. Pavlikov, and D. Kritskiy (Eds.), Integrated Computer Technologies in Mechanical Engineering - 2020, Vol. 188, Springer, Cham (2021), pp. 609-619. https://doi.org/10.1007/978-3-030-66717-7_52
5. D. V. Akimov, V. Z. Gryshchak, S. I. Gomenyuk, et al., “Finite-element analysis and experimental investigation on the strength of a three-layer honeycomb sandwich structure of the spacecraft adapter module,” Strength Mater, 48, No. 3, 379-383 (2016). https://doi.org/10.1007/s11223-016-9775-y
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