AE661 : Buckling and Post-buckling in Aircraft Structures

Department

Department of Aeronautical Engineering

Academic Program

Master in Master of Aerospace Engineering

Type

Elective

Credits

03

Prerequisite

Overview

Buckling of thin plates, Post-buckling of plates and stiffened panels. Failurecriteria following semi-empirical approach. Needham and Gerard methods forpredicting the failure stresses. Buckling of cylindrical shells subjected to individual orcombined external and axial compressions.