1.

A fuselage is configure to have length L. What will be the approximated internal volume (V)?

A. V = 3.4*(S<sub>top</sub>*A<sub>side</sub>/4L)
B. V = 3.4/4L
C. V = 3.4*(S<sub>top</sub>*A<sub>side</sub>/4)
D. V = 0.4*(S<sub>top</sub>*A<sub>side</sub>/L)
Answer» B. V = 3.4/4L


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