MCQOPTIONS
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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 | |