Work

Stability of the Cantilever Elliptical Composite Cylindrical Shell during Transverse Bending

Year: 2025

Type: article

Source: Russian Aeronautics

DOI: 10.3103/s1068799825030043

Author: L. P. Zheleznov

Institutions: Siberian Aeronautical Research Institute Named After S.A. Chaplygin, Siberian Transport University

Language: English

Topic: Composite Structure Analysis and Optimization

Subfield: Mechanics of Materials

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W7128818256

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Cites: 4

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