ENGG 146 - Aircraft Structures

Semester 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.