Composite Fuselage Proposal—Part 1: Static and Modal Finite Element
Analysis
S. Sulthan,
K. Balaji,
C.K. Akhil
et al.
Abstract:<div class="section abstract"><div class="htmlview paragraph">The objective of this paper is to analyze a complete fuselage of an airplane made
of composite materials. The analysis presented includes designing a 3D fuselage
structure in which parameters are calculated using various stress and
deformation scenarios. Static numerical results propose a composite fuselage
structure to reduce stress and deformation levels by… Show more
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