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Nov 22, 2024
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ENGG 146 - Aircraft StabilitySemester Hours: 3
Periodically
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.
Prerequisite(s)/Course Notes:
ENGG 028 , MATH 131 . (Formerly Aircraft Structures.)
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