[1]
Ramadhan, R.A. et al. 2020. A FINITE ELEMENT ANALYSIS OF CRITICAL BUCKLING LOAD OF COMPOSITE PLATE AFTER LOW VELOCITY IMPACT. Indonesian Journal of Aerospace. 18, 2 Desember (Dec. 2020), 105–116. DOI:https://doi.org/10.30536/j.jtd.2020.v18.a3328.