Stress analysis of splice joint of the aircraft bottom wing skin by Finite Element Method
Year: 2024
Type: conference-paper
Authors: Rajesh Kumar N, Gokul S, Uday V, Vishwa M
Language: English
Topic: Engineering Applied Research
Subfield: Civil and Structural Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4404836378