Consider an aircraft with a maximum take-off weight of 1284 kg, a wingspan of 6.3 m, and a wing area of 27 m2. What is its calculated wing loading?
Wing loading is denoted by W ÷ S.
It describes how much weight is districuted per unit of wing area (how much lift must be produced).
Given:
- MTOW = 1284 kg
- Wing area = 27 m2
Wing Loading = 1284 kg ÷ 27 m2 = 47.55 kg/m2
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