Designing Ailerons for School Project Wing

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pegus
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Good day everyone, I was designning the wing for a school project and I wonder if there is any equation for defining the aileron size. I am designing a straight rectangular wing. I just found on other forums that the aileron's length should be 0.25 of the wingspan and the aileron chord should be 0.25 of the wing mean chord.
 
on Phys.org
Raymer's Aircraft design; A conceptual approach and Anderson's Aircraft performance and design have lots of information.
 
I'm sure comparing a bunch of wings will eventually yield a value you could use but the speed it is designed to operate might factor in.