On the static aeroelastic tailoring of composite aircraft swept wings modelled as thin-walled beam structures-Reference-Cited by-同舟云学术

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On the static aeroelastic tailoring of composite aircraft swept wings modelled as thin-walled beam structures

Published:1992-01 Issue:5-7 Volume:2 Page:497-512
ISSN:0961-9526
Container-title:Composites Engineering
language:en
Short-container-title:Composites Engineering

Author:

Librescu Liviu,Song Ohseop

Publisher

Elsevier BV

Subject

General Engineering

Reference32 articles.

1. Vibrations of composite thin-walled beams with designed-in elastic couplings;Atilgan,1990

2. Composite box beam analysis: Theory and experiment;Bauchau;J. Reinf. Plastics Compos,1987

3. Aeroelastic behavior of forward swept graphite/epoxy wing aircraft with rigid body freedoms;Chen,1986

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