Open AccessTooling Design Modeling for Composite Fuselage of Beechcraft King Air 250 using CATIA
Author(s) -
Miazor Fidelis Ekom
Publication year - 2021
Publication title -
journal of aviation technology and engineering
Language(s) - English
Resource type - Journals
ISSN - 2159-6670
DOI - 10.7771/2159-6670.1211
Subject(s) - fuselage , composite number , process (computing) , stiffness , aerospace , specific modulus , structural engineering , mechanical engineering , specific strength , engineering , computer science , automotive engineering , materials science , aerospace engineering , composite material , operating system