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Understanding load distribution is critical in structural design from "summary" of Aircraft Structures & Systems EASA Module 13 B2 by

Load distribution is a critical aspect of structural design, particularly in the context of aircraft structures. The distribution of loads across a structure plays a crucial role in ensuring the overall structural integrity and safety of the aircraft. Understanding how loads are distributed throughout an aircraft is essential for engineers and designers to create a structure that can withstand the various forces it will encounter during flight. In aircraft structures, loads can be distributed in a variety of ways, including through bending, torsion, shear, and compression. Each of these load distribution mechanisms has its own unique characteristics and effects on the structure. For example, bending loads can cause the structure to flex, while torsional loads can twist it. By understanding how these different types of loads are distributed throughout the structure, engineers can design a structure that is capable of withstanding the stresses it will face during ...
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    Aircraft Structures & Systems EASA Module 13 B2

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