E, 63% of the value. I forget the rationale behind it but I learnt that in engineering. 90% confident for that answer.
Answer:
So lift will be 30.19632 N
Explanation:
We have given area of the wing
We know that density of air
Speed at top surface and speed at bottom surface
According to Bernoulli's principle force is given by
Vector 1 has components
and vector 2 has
Add these vectors to get the resultant, which has components
The magnitude of the resultant is
with direction such that
or about 50º N of E.
So i believe is exercise:)