This article is maintained by: Elsevier
Article Title: Conceptual design and simulation validation based finite element optimisation for tubercle leading edge composite wing of an unmanned aerial vehicle
Journal Title: Journal of Materials Research and Technology
CrossRef DOI link to publisher maintained version: https://doi.org/10.1016/J.JMRT.2019.07.049
Content Type: article
Copyright: © 2019 The Authors. Published by Elsevier B.V.