Search results for query: *

75 is exact fiber Young's Modul but for result you have to use the Mixure teory. that means Elaminate = Efiber*Vfiber+Ematrix*Vmatrix 73 * 0.171 + 3*0.829 = 73 GPA i havent find any other output. i hope this has help you....

hi Stanley the only problem with the thesis is the language, it is in Slovak language,now im preparing for final state examination(B.A.)-17th of june 2005 i was not having time to translate it into English. may be during the next few weeks i will have the time for it. but maybe you will...

the best book, i've have read about composite material was: Mechanics of composites material Robert M. Jones second edition Vladimir zachar just finish the school, what now? http://www.madmonkey.ahoj.sk/madmonkey.html

Hi tstanley i have already done the "research". but lets start with answer of your questions. material was woven, but there is "no" different. cause sample look like: |`````\_____/``````| | |_____/`````\______| and the middle fibers what are perpendicular to tensile force has almost none...

Drej The equation you wrote is not the rightone, cause it doesnt envisage height of the layer. the best solution what i have found yet is the mixure rule for composite material(for 1 layer), but i can use it cause the composite is made only from 2 components. E=Ef*Vf+Em*Vm where Vf and Vm...

hi all ansys fan i have model of Uni Directional composite material. 3-14 layers matrix fiber matrix fiber .. element solid46 + relative thickens for layers(volume fraction) tensil pressure material(matrix, fiber) properties E(young modulus) poissons constants problem is: after solving i can...

Thank you harry this was the first step, and it helps, another problem is to display the stress-strain graph for all the layer like a composit. all i can do now is to choose the element and than the node.and i get the E of the layer what is nearest the node(top or botton). now i got 2 lines...

hi all ansys fan, my problem: i have solved cantilever(console) made of composite material(3layers) - tensioned, but i dont know how to find out the stress for the 2nd layer(middles layers). i dont know how to find out the total stress for whole element. i can get stress only from the top and...

madmonkey (Automotive) 16 May 05 14:15 HI ALL i am trying to simulate in ANSYS the Tension Strength Test (TST).The TST has been already done. i got the values(grapf stress-strain). Now im traing to create the simulation of the TST in ANSYS. I got all the materials values: fiber E=73GPa...

HI ALL i am trying to simulate in ANSYS the Tension Strength Test (TST).The TST has been already done. i got the values(grapf stress-strain). Now im traing to create the simulation of the TST in ANSYS. I got all the materials values: fiber E=73GPa, V(volume)fiber=0.32 Poisson=0.25 matrix...

HI ALL i am trying to simulate in ANSYS the Tension Strength Test (TST).The TST has been already done. i got the values(grapf stress-strain). Now im traing to create the simulation of the TST in ANSYS. I got all the material values: fiber E=73GPa, V(volume)fiber=0.32 Poisson=0.25 matrix e=3Gpa...