The depth of the crack along the aeroplane wing is determined as 1.5 m.
The depth of the crack in the wing from which the echo is heard is calculated as follows;
d = (vt)/2
From the image;
d1 = (5000 x 0.4 x 10⁻³)/2
d1 = 1 m
d2 = (5000 x 0.8 x 10⁻³)/(2)
d2 = 2 m
Average depth
d = (d1 + d2)/2
d = (1 + 2)/2
d = 1.5 m
Thus, the depth of the crack along the aeroplane wing is determined as 1.5 m.
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