Zobrazeno 1 - 8
of 8
pro vyhledávání: '"E. F. Chesmar"'
Publikováno v:
Journal of Materials Science. 38:2547-2555
Thirteen commerical wing panels were fabricated and flown on a commercial aircraft to investigate the mechanisms of water migration through various honeycomb cores. A 12.2 J impact damage was not observed to cause damage propagation in aluminum and K
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::13ef1dada1e6cc552ebe8a3a20b77fef
https://doi.org/10.1023/a:1023985925293
https://doi.org/10.1023/a:1023985925293
Publikováno v:
Journal of Materials Engineering and Performance. 8:661-668
When honeycomb composite structures are fabricated for the aerospace industry, they are designed to be closed to their operating environment for the life of the composite structure. However, once in service, this design can break down. Damage can set
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ffbe5438a2e89c530c22607adfefaed9
https://doi.org/10.1361/105994999770346422
https://doi.org/10.1361/105994999770346422
Autor:
Shafizadeh, J. E.1, Seferis, J. C.1 seferis@cheme.washington.edu, Chesmar, E. F.2, Frye, B. A.3, Geyer, R.3
Publikováno v:
Journal of Materials Science. Jun2003, Vol. 38 Issue 11, p2547-2555. 9p.
Publikováno v:
Macromolecular Chemistry & Physics; Feb2005, Vol. 206 Issue 3, p393-403, 11p
Autor:
Ahn, Sung-Hoon, Springer, George S.
Publikováno v:
Journal of Composite Materials; Jun1998, Vol. 32 Issue 11, p1036-1074, 39p
Autor:
Ischdonat, Nils
The accomplished study is based on the appointment and identification of ageing effects and according to this absorption of moisture of aircraft cabin components over the life-cycle. In the first step of the study ceiling panels from same age and fro
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::261d589344eabe36a9ca8d7178823cee
Autor:
Senthilkumar Krishnasamy, Chandrasekar Muthukumar, Senthil Muthu Kumar Thiagamani, Sanjay Mavinkere Rangappa, Suchart Siengchin
A composite sandwich panel is a hybrid material made up of constituents such as a face sheet, a core, and adhesive film for bonding the face sheet and core together. Advances in materials have provided designers with several choices for developing sa
The papers from these proceedings address experimental and analytical methods for the characterization and analysis of modern composite and adhesive systems. They have been produced to provide understanding that can be used to design safe, reliable e