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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 | |