[1]
Lam, X.-B. 2020. Multidiscilinary design optimization for aircraft wing using response surface method, genetic algorithm, and simulated annealing. Journal of Science and Technology in Civil Engineering (JSTCE) - HUCE. 14, 1 (Jan. 2020), 28-41. DOI:https://doi.org/10.31814/stce.nuce2020-14(1)-03.