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MIL-HNBK-17 would be a good source for both micro-mechanics models for lamina properties and laminated plate theory. -wade "Matt Oliverius" <[EMAIL PROTECTED]> wrote in message news:[EMAIL PROTECTED] > Hi all, > > I am trying to calculate composite moduli for a (45/45/45/45) laminate in 1 > degree increments from 0 to 360 degrees. However, the equations I am > finding in textbooks are undershooting the modulus. For example suppose my > fiber modulus (E) is around 20MSI and my matrix modulus (E) is 1 MSI. Then > when I plug theta of 45 into a transformation equation (assuming 0 is the L > direction of the composite), then I come up with a modulus of 2MSI, when it > should be around 20MSI. Does anyone know what might be wrong? Is there an > assumption about the stackup in these equations that I might be missing? > If so, where can I find references to the generalized solution E = f(theta) > for any stackup? > >
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