| |
May 03, 2024
|
|
|
|
|
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.
Add to Personal Catalog (opens a new window)
|
|