Can someone use other dimensions they know of the A380 wing and approximate what this area would be, we can say that these 3 sections are rectangular and we can also add 20% to estimate the area added by slats which we can't see in the video.
It would be ideal if I knew the chord length and then I could use the logger pro software to find the width of the rectangle but I have been unable to find this data, even from Airbus because the A380 project is closed.
link to video:
Please someone help me, with this information I will able to do all the maths I am doing using related rates to model the rate of change of lift of an A380 after take-off (basically this additional area will help me get dA / dt where A is area and t is time, it's useful because its a related rate to lift as Planform area is in the lift equation.)
I have tried for days and not been able to get this number, I would appreciate any assistance from you online folks. Even any approximate number is useful please, just get me a reasonable number and also explain how you did it.