Abstract
Laminated fibrous composite beams and plates are finding an increasing use in aerospace, marine, mechanical, and other branches of engineering. In order to achieve a better understanding and to identify the key areas of research and the potential problems of analysing composite materials, a review of the relevant literature is presented in this paper. Particular emphasis is given to the development of the optimisation of dynamic stress and aeroelastic tailoring efforts in laminated composite beams with both geometric and material coupling between the bending and torsional deformations. The effects of axial load, transverse shear deformation, rotatory inertia and the fibre orientation are reviewed.
Original language | English |
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Title of host publication | Proceedings of the AERO 2000 First International & Third Bi-Annual Conference of the Iranian Aerospace Society |
Place of Publication | Tehran, Iran |
Publisher | Sharif University Press |
Pages | 397-407 |
Number of pages | 11 |
Volume | 4 |
Publication status | Published - Dec 2000 |
Event | Proceedings of the AERO 2000 First International & Third Bi-Annual Conference of the Iranian Aerospace Society - Tehran, Iran, 2000 Duration: 1 Dec 2000 → … |
Conference
Conference | Proceedings of the AERO 2000 First International & Third Bi-Annual Conference of the Iranian Aerospace Society |
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Period | 1/12/00 → … |
Keywords
- Laminated fibrous composite
- vibration
- aeroelastic tailoring