Finite element methodologies development to simulate the behaviour of composite fuselage structure and correlation with drop test

Author: Wiggenraad J.F.M.   Michielsen A.L.P.J.   Santoro D.   Lepage F.   Kindervater C.   Beltran F.   Al-Khalil M.  

Publisher: Elsevier

ISSN: 1290-0958

Source: Air & Space Europe, Vol.3, Iss.3, 2001-05, pp. : 228-233

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

Previous Menu Next

Abstract