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Fall 2024
Jul 13, 2024
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Information Select the Course Number to get further detail on the course. Select the desired Schedule Type to find available classes for the course. The Schedule Type links will be available only when the schedule of classes is available for the selected term.

AAE 35200 - Structural Analysis I
Credit Hours: 3.00. Properties of wing and fuselage sections. Beam-column moments. Torsion of thin-walled and skin-stringer multiple-cell sections. Nonsymmetrical bending of skin-stringer wing sections. Flexural shear in open and closed thin-walled and skin-stringer sections. Loads and stresses in the rib system. Cutouts and shear lag. Modified beam theory for wing and fuselage design. Deflection by energy method. Introduction to composite structures.
3.000 Credit hours

Syllabus Available
Levels: Undergraduate, Graduate, Professional
Schedule Types: Distance Learning, Lecture

Offered By: School of Aero and Astro Engr
Department: Aeronautics & Astronautics

Course Attributes:
Upper Division

May be offered at any of the following campuses:     
      West Lafayette

Learning Outcomes: 1. Use analytical/empirical tools for determining the distribution of load (or displacement) in typical aerospace components. 2. Understand and implement the procedures for relating applied loads (or displacements) to component "failure". 3. Select of materials to resist structural failure. 4. Be exposed to other professional development topics are also to be presented as time permits (e.g., technical communications, teamwork issues, economic considerations, engineering ethics, case histories, regulatory and certificiation, topics, etc.).

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