calculating vertical deflections on T section Beam using stand7 and compare with theory

Details:
Case study is Finite Element Investigation of Cantilevered Beam (T-Section)
I did a lab test to calculate the vertical deflections of a T-section cantilevered beam which is fixed at one end and subjected to vertically downward points load at the of free end I applied different loads in N to the beam, Ive taken data using Digital dial indicators on 7 locations along the beam applying loads starting from 18N then 50 then adding 50N until I get to 800N
Measurements:
Beam length is 980mm
Flange width is 102 mm flange thickness is 8.4 mm
Web is 118 mm Web thickness is 6.4 mm
Youngs modulus value is 200 KN/mm2

I need to compare those results I got from the lab with whats below:

1-Theory I need to use double integration ( Macaulay’s method) to find the vertical deflection along the top surface of the beam. I dont want all calculations for each load and section but I would like to do examples on theory calculations on 100N, and 800N for all 7 sections showing the formula being used to do that

2-Using Strand 7 design software to calculate vertical deflections along the top surface, bending and stress this time for 100N 200N 300N then 550N 650N then 800N

Work in unite for stand7 is N (Force) and mm (length) and MPa (=N/mm2 modulus/stress)
Use plate/shell QUAD8 element
Use 32 or more elements to get to the nearest results to theory and lab
Plot a graph with the span wise finite element deflection values superimposed on the theoretical and lab values

I will send you my lab results in Excel and so you add theory results and Strand7 to the table .. You can organise it in the best you find suitable.

I hope thats this information are clear if not please let me know many thanks