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Academic Year: | 2013/4 |
Owning Department/School: | Department of Mechanical Engineering |
Credits: | 6 |
Level: | Masters UG & PG (FHEQ level 7) |
Period: |
Semester 1 |
Assessment: | CW 33%, EX 67% |
Supplementary Assessment: |
Like-for-like reassessment (where allowed by programme regulations) |
Requisites: | Before taking this unit you must take ME30045 |
Description: | Aims: To introduce advanced techniques of analysis and design of aircraft structures. Learning Outcomes: After taking this unit the student should be able to: * Analyse buckling of struts and composite panels. * Analyse post-buckling behaviour of simple structural systems and stiffened panels. * Understand the principles of aeroelasticity and wing divergence * Formulate structural optimisation problems. * Describe various optimisation methods applicable to structural designs. * Use appropriate optimisation methods to design structures for given requirements. Skills: Problem solving; mathematical modelling; numeracy; written communication; IT; working independently. Content: Buckling and post-buckled stability of simple structural systems. Introduction to aeroelasticity. Wing divergence. Buckling analysis and design of composite structures. Analysis of post-buckled stiffened panels. Formulation of structural optimisation problems. Optimisation methods in structural designs: mathematical programming and heuristic methods. |
Programme availability: |
ME40220 is Optional on the following programmes:Department of Mechanical Engineering
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