Tropical Natural Fibre Composites

Author: Mohd Sapuan Salit
Publisher: Springer
ISBN: 9812871551
Size: 15.64 MB
Format: PDF, ePub
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Anuar, H., Sapuan, S.M.: Durian skin fibre and its composites. In: Proceedings of
Postgraduate Symposium on Composites Science and Technology 2014, 28 Jan,
pp. 1–4. Putrajaya, Malaysia (2014) 2. Dorworth, L.C., Gardiner, G.L., Mellema,
G.M.: Essentials of Advanced Composite Fabrication and Repair. Aviation
Supplies & Academics Inc, Newcastle (2009) 3. Easterling, K.: Tomorrow's
Materials, 2nd edn. The Institute of Materials, London (1990) 4. Gordon, J.E.: The
New Science ...

Composite Materials

Author: S.M. Sapuan
Publisher: Butterworth-Heinemann
ISBN: 0128026456
Size: 66.33 MB
Format: PDF, Kindle
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Engineering Design, fourth ed. McGraw-Hill Companies, Inc, Boston. Dorworth,
L.C., Gardiner, G.L., Mellema, G.M., 2009. Essentials of Advanced Composite
Fabrication & Repair. Aviation Supplies & Academics, Inc, Newcastle,
Washington. Eastwood, M.D., Haapala, K.R., 2015. A unit process model based
methodology to assist product sustainability assessment during design for
manufacturing. J. Cleaner Prod. 108,54–64. Fuad-Luke, A., 2009. EcoDesign,
The Sourcebook, third ed.

Journal Of Advanced Materials

Author:
Publisher:
ISBN:
Size: 39.39 MB
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Design of Durable, Repairable, and Maintainable Aircraft Composites, lSBN
Number: 978-0-7680-0020-7. Available from the SAE Commercial Aircraft
Composite Repair Committee (CACRC) atwww.sae.org; document reference AE-
27 Dorworth, L., Gardiner, G., and Mellema, G.; Essentials of Advanced
Composite Fabrication and Repair, in print. Figure 22. Inspect Repair — Top skin
(top) and bottom skin (bottom) surfaces are inspected. Note use of repair tooling
in restoring curvature ...

Bonded Repair Of Aircraft Structures

Author: A. Baker
Publisher: Springer Science & Business Media
ISBN: 9400927525
Size: 41.49 MB
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The use of adhesive bonding in aircraft structure has expanded greatly in recent
years as more and more advanced composite materials are being utilized. In
general, the most efficient composite to metal splice joints have been scarf and
stepped lap joints in which there is relatively little change in the load path. With
this increased use of bonded assemblies comes the increased potential for
processing anomalies, mistakes during fabrication, and in service damage.
Repair methods ...