Given:
\(A = 80 \, \text{m}^2\)
Using Bernoulli’s equation:
\(\Delta P = (P_2 - P_1) = \frac{1}{2} \rho (V_1^2 - V_2^2)\)
Area of wings = \(A\)
Calculating the lift force:
\(mg = \frac{1}{2} \times 1 \times (70^2 - 50^2) \times 80\)
Simplifying:
\(mg = 40 \times 2400\)
\(m = 9600 \, \text{kg}\)