Module 4: Plane Stress Constitutive Equations
  Lecture 15: Lamina Engineering Constants
 


Axial Modulus
:


Consider a unidirectional off axis lamina. This lamina is subjected to the loading  and  as shown in Figure 4.2.
Thus, from Equation (4.5) for this state of stress we can write the axial strain as

(4.61)

The Young’s modulus in x-direction is now defined as

(4.62)

Thus, from Equation (4.61), we can write

(4.63)

Figure 4.2: Off axis lamina loaded in traction along x direction

In the above equation,  is written using compliance terms in principal material directions as

(4.64)

Further, it can be writing compliance terms in principal directions using engineering constants doing some rearrangements as

(4.65)

From this expression it is easy to see that the modulus  when   and  when . The variation of the modulus  with fibre orientation for AS4/3501-6 Epoxy material is shown in Figure 4.3. The variation of the modulus  for both positive and negative fibre orientations is identical in nature.

Figure 4.3: Variation of axial modulus with fibre orientation for AS4/3501-6 Epoxy


Axial Poisson’s Ratio:

The axial Poisson’s ratio  can also be obtained for above loading condition. This Poisson’s ratio is defined as

(4.66)

Using Equation (4.61) we can write

(4.67)

Further, expressing the compliance terms in above equation in terms of engineering constants we can write

(4.68)