A fuselage is configure to have length L. What will be the approximated internal volume (V)?(a) V = 3.4*(Stop*Aside/4L)(b) V = 3.4/4L(c) V = 3.4*(Stop*Aside/4)(d) V = 0.4*(Stop*Aside/L)The question was asked during an interview.I would like to ask this question from Configuration Layout in portion Configuration Layout and Loft of Aircraft Design

A fuselage is configure to have length L. What will be the approximate

1.	A fuselage is configure to have length L. What will be the approximated internal volume (V)?(a) V = 3.4(StopAside/4L)(b) V = 3.4/4L(c) V = 3.4(StopAside/4)(d) V = 0.4(StopAside/L)The question was asked during an interview.I would like to ask this question from Configuration Layout in portion Configuration Layout and Loft of Aircraft Design
Answer» Right OPTION is (a) V = 3.4(StopAside/4L) The explanation is: Internal volume of FUSELAGE will be total available volume for crew, cargo, passenger etc. Typically, from side and TOP VIEW we can estimate internal volume. If area of side is Aside and area of top is Stop then, internal volume is given as, V = 3.4(StopAside/4L), where L = LENGTH of the fuselage.

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