units
MAE1042
Faculty of Engineering
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6 points, SCA Band 2, 0.125 EFTSLRefer to the specific census and withdrawal dates for the semester(s) in which this unit is offered.
SynopsisThis unit will introduce the student to aircraft structural analysis. Concepts of load paths, equilibrium, forces/moments, stresses/strains, reaction forces and bending moments will be presented. Basic trusses and beam analysis will be used to analyse simple airframes. Students will trace the historical development of the airframe from truss-like structures to modern semi-monocoque construction and the importance of appropriate material selection. The concept of static structural equilibrium will be extended to consider 'dynamic equilibrium' through the introduction of mechanical vibrations. The last two weeks will introduce basic concepts of orbital mechanics/spaceflight followed by an introduction to rocket propulsion. Objectives
Assessment
Field Trip (10%), Structures laboratory (10%), Exam (80%) Chief examiner(s)Contact hours5 contact hours per week, 7 non-contact hours per week. PrerequisitesNone Co-requisitesProhibitions |