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Vue d'ensemble
G茅nie m茅canique : Aircraft structural components and loads. Bending, shear and torsion of thin-walled open and closed beams. Structural idealization. Wing spars and box beams. Wings bending, torsion and shear, tapered wings, deflection, cut-outs. Fuselage frames and wing ribs, principle of stiffener/web construction. Analysis of riveted, bolted and adhesive joints. Sandwich structures analysis.
Terms: Hiver 2011
Instructors: Hubert, Pascal (Winter)
- (3-0-6)
- Prerequisite: MECH 321 or equivalent
- Restriction: Not open to students who have taken MECH 432.