Title: Failure mechanisms of laminates transversely loaded by bolt push-through
First published: 1985
Subjects: Adhesive bonding, Airframes, Airplanes, Bolted joints, Bolts, Composite materials, Failure modes, Fatigue, Fuselage, Fuselages, Interlayers, Laminates, Loads (Forces), Panels, Stiffening, Toughness, Wing panels