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Please note that this OpenCourseWare platform will be replaced at the end of 2026 by a new platform (under the same url ocw.tudelft.nl).

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4.5.2 Lecture: Wing Spars

Course subject(s) Module 4. Loads and Stresses

In the previous lectures, we have analyzed the strains and stresses due to two loading cases for the fuselage structure. We would also like you to understand the strains and stresses in a wing structure. What is a typical loading case for wing structures during flight? Wing bending. In this last lecture we will look into the function of the spar elements in the wing and how they transfer loads and stresses in the structure.

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Introduction to Aerospace Structures and Materials by TU Delft OpenCourseWare is licensed under a Creative Commons Attribution-NonCommercial-ShareAlike 4.0 International License.
Based on a work at https://online-learning.tudelft.nl/courses/introduction-to-aerospace-structures-and-materials/.
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