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Feb 10, 2025
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ENGG 146 - Aircraft Structures
Once every three semesters
Analysis of semimonocoque structures as typified by aircraft wings and fuselages. Normal stress and shear stress analysis of non-symmetric cross-sections, applications to open and closed box thin-walled beams with longitudinal stiffeners. Effects of taper. Torsion of closed box beams, multiple cell beams.
Prerequisites & Notes
ENGG 28, MATH 131. No liberal arts credit.
Credits: 3 s.h.
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