Aero-structural numerical analysis of a blended wing body unmanned aerial vehicle using a jute-based composite material

Conference Object

Abstract: Research and development of biocomposites for Unmanned Aerial Vehicle (UAV) structures have become r

Palabras claves:

Finite Element Method, Flight loads, Jute Fiber Composite, Semi-monocoque structure, Unmanned aerial vehicle

Autores:

Carlos W. Díaz-Campoverde, Cristian Cruzatty, Edgar H. Cando, Edgar Sarmiento, Esteban Valencia, José Rivera

Fuentes:

scopus