Hi SW, I have no particular customer requirement. I just want to find out how my composite material performance under thermal shock condition. I was thinking of plunging the test samples into a chamber set at, say -50C, leave for 5-10 minutes and move them to hot chamber, say 100C, leave for...
Hi SWComposites,
I need to investigate if my composites are prone to matrix cracking or other failure mode when subject to thermal shock during flights.
Compositepro - what causes the increase in internal stresses and the brittleness?
Swcomposites - is the reduction in the compression strength resulted from increase in the weaviness of ply due to heavier tow (i.e. 12K fibre)??
RPstress & all - what ifI use a combination of different gsm fabric...
Gents,
I have a PMMA screen of around 800mm x700mm and 6mm thick. If I were to scored the sheet 3mm deep of v shape grove and from one corner of the sheet to another in the form of X. If the sheet is then subjected to impulse pressure of @ 20KPa. Do you think the sheet will break into small...
Thanks for all your contributions. I guess the general opinions are analysis is difficult and inaccurate and best is to carry out appropriate testing.
Thanks again
Thanks for the feedback gents, but what if I have to use the composite above its Tg, does the FE analysis result which generated from non linear test data is still appropriate?? may be I should look into FE analysis on elastomeric materials??
Has anyone has any experience in using composite material above its Tg. If one could characterise its mechanical properties (at temperature >Tg and ignoring non linear failure behaviour), can one use them for FE analysis i.e. does the FE result applicable or appropriate??
n/b: the component...
Compositepro, do you think ILS determined from a flat laminate can be used to analyse a tube structure like a pipe? also if the pipe is subject to a bending load will there be any shear load in the NA of the pipe and how far off the ILS of the pipe from ILS determined from flat laminate?