DELAMINATION DURING BUCKLING OF COMPOSITE CONSTRUCTIONAL ELEMENTS | Zendy

Antanas Žiliukas | Zendy

AI Assistant Blog Pricing

Home ZAIA Blog

Open Access

DELAMINATION DURING BUCKLING OF COMPOSITE CONSTRUCTIONAL ELEMENTS

Author(s) -

Antanas Žiliukas

Publication year - 2010

Publication title -

aviation

Language(s) - English

Resource type - Journals

SCImago Journal Rank - 0.239

H-Index - 13

eISSN - 1822-4180

pISSN - 1648-7788

DOI - 10.3846/aviation.2010.06

Subject(s) - buckling , delamination (geology) , composite number , structural engineering , shear strength (soil) , stress (linguistics) , materials science , aerospace , composite material , shear (geology) , engineering , aerospace engineering , geology , paleontology , linguistics , philosophy , soil water , soil science , subduction , tectonics

Laminated constructional elements have widespread applications in aerospace. This paper presents of the buckling for E‐Glass. Design solution based by the criteria of strength materials. The delamination of composite constructional elements is determined by the normal and shear stress. The non‐linear strength criterion suggested by the author in case of complex state of stress. Santrauka Kompozitiniu konstrukciju elementu atsisluoksniavimas nustatomas remiantis normaliniais ir tangentiniais itempiais. Autorius siūlo netiesini stiprumo kriteriju, ivertinanti sudetinga itempiu būvi sprendžiant kompozitu atsisluoksniavimo problema.

The content you want is available to Zendy users.

Already have an account? Click here to sign in.

Having issues? You can contact us here

Accelerating Research