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This document provides details for an exercise on fuselage design for an aerospace structures course. The goals are to understand load carrying mechanisms in a fuselage and estimate loads on structural components to minimize weight. Specifically, it involves calculating shear, bending, and torsional loads along a Cessna 172 fuselage given assumptions about mass distributions and flight conditions. It also involves calculating loads in the fuselage

Author

Indra Furwita

Language

EN