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Academic Year: | 2014/5 |
Owning Department/School: | Department of Mechanical Engineering |
Credits: | 6 |
Level: | Honours (FHEQ level 6) |
Period: |
Semester 1 |
Assessment Summary: | CW 25%, EX 75% |
Assessment Detail: |
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Supplementary Assessment: |
ME30045 Re-Assessment Examination (where allowed by programme regulations) |
Requisites: | |
Description: | Aims: To introduce appropriate techniques for the loading, stress analysis and failure prediction of aircraft structures. Learning Outcomes: After taking this unit the student should be able to: * Determine critical gust and manoeuvre load cases for an aircraft. * Construct shear force, bending moment and torque diagrams. * Design aircraft structures by accounting for static strength, buckling and fatigue failure. Skills: Problem solving; numeracy; working independently; written communication. Content: Influence of speed, altitude, geometry, weight and stiffness on aircraft loads. Gust and manoeuvre envelope. Shear force, bending moment and torque diagrams. Shear flow and shear centre of open and close sections. Fracture strength and crack propagation, including safe-life and damage-tolerant design. Shear buckling and tension fields - analysis and design of ribs and spars. Compression buckling of stiffened panels - analysis and design of wing panels. Introduction to structural optimisation. |
Programme availability: |
ME30045 is Compulsory on the following programmes:Department of Mechanical Engineering
ME30045 is Optional on the following programmes:Department of Mechanical Engineering
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