[1]
Fauzi, A.F., Pratama, M.R. and Silalahi, N. 2025. Structural analysis of the Wing of UCAV (Unmanned Cargo Aerial Vehicle) using finite element method. International Journal of Mechanical Computational and Manufacturing Research. 14, 2 (Aug. 2025), 97–106. DOI:https://doi.org/10.35335/computational.v14i2.273.