๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

The use of composites in aircraft primary structure

โœ Scribed by W.T. Freeman


Publisher
Elsevier Science
Year
1993
Weight
717 KB
Volume
3
Category
Article
ISSN
0961-9526

No coin nor oath required. For personal study only.


๐Ÿ“œ SIMILAR VOLUMES


The use of neutron imaging for the study
โœ P.C. Hungler; L.G.I. Bennett; W.J. Lewis; J.S. Brenizer; A.K. Heller ๐Ÿ“‚ Article ๐Ÿ“… 2009 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 245 KB

Highly maneuverable aircraft, such as the CF188 Hornet, have several flight control surfaces on both the leading and the trailing edges of the wing surfaces. They are composed of composite panels constructed of aluminum honeycomb core usually covered with graphite epoxy skins. Although very light an

Use of graphics in an aircraft design of
โœ W.A. Coles ๐Ÿ“‚ Article ๐Ÿ“… 1977 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 682 KB

This paper describes the computer-aided design/computer aided manufacture system which has been developed by the Military Aircraft Diviยข.io.:7 of the British Aircraft Corporation. Its uses and current developments are outlined. The system supports batch, timesharing, and fully interactive graphic pr

Investigation of structure/property rela
โœ C. A. Cooper; R. J. Young ๐Ÿ“‚ Article ๐Ÿ“… 1999 ๐Ÿ› John Wiley and Sons ๐ŸŒ English โš– 609 KB

Raman spectroscopy has been used to characterise the structure of three very different particulate composite systems: aramid particles in nylon 6.6, cast iron (graphite particles in an iron matrix) and C 60 or carbon nanotubes in an epoxy resin matrix. In addition, Raman spectroscopy has been used t

Finite element analysis of cracks in agi
โœ Linxia Gu; Ananth Ram Mahanth Kasavajhala; Shijia Zhao ๐Ÿ“‚ Article ๐Ÿ“… 2011 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 609 KB

Bonded composite-patch repair has been used to transfer load from cracked structures to the reinforcement such that subsequent crack propagation is reduced. In this study, the mechanical behavior of a single edge v-notch Al7075-T6 plate repaired with 1-ply and 4-ply composite patches was investigate