Yes, you'd need another formula to calculate the stress, \sigma, at different places in the section.
Stress is defined as force divided by the area, and strain,\epsilon, is the unit deformation, i.e. deformation divided by the length.
In the absence of axial forces, the stress at the neutral axis is zero, therefore the strain also.
The stress,\sigma, is given by the formula:
\sigma=Mc/I, where
M=bending moment,
I=moment of inertia of cross section, and
c=distance from neutral axis.
This means that the further away from the neutral axis, the greater is the stress. This formula assumes plane stress, meaning that the deformations across the section remain in a plane.
The strain at different points is simply
\epsilon = \sigma/E, where E is the modulus of elasticity.
You said you have obtained the neutral axis. Did you calculate the moment of inertia of the section? What did you get?
Just a side question: do you have any textbooks on Strength of Materials? If not, I can recommend a few that you can certainly get from the library:
Strength of Materials, by Stephen Timoshenko (the classic, but rather expensive)
https://www.amazon.com/dp/0898746213/?tag=pfamazon01-20
Strength of Materials, by J. P. Den Hartog, an excellent work, available in Dover edition
https://www.amazon.com/dp/0486607550/?tag=pfamazon01-20
Strength of Materials, By Pytel and Singer, a standard textbook, very affordable.
https://www.amazon.com/dp/0060453133/?tag=pfamazon01-20