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COURSE PRO FORMA




            IMPORTANT:
            Contents of this Pro Forma shall not be changed without the Senate’s approval for items indicated with *. Changes
            to the other items can be approved at the Academy/Faculty/Institution/Centre level.

           Academy/Faculty/Institute/Centre      Faculty of Engineering

           Department                            Mechanical Engineering
           Programme                             Bachelor of Materials Engineering
           Course Code*                          KMEB 4346

           Course Title*                         Aerospace Materials
           Course Pre-requisite(s)/ Minimum Require-  None
           ment(s)
           Student Learning Time (SLT)*          120

           Credit*                               3
           Course Learning Outcomes*             By end of this course, student are able to:
                                                 1.  Relate properties of aerospace materials with stresses acting on air-
                                                     craft during flight.
                                                 2.  Compute fluid (air) pressure difference and hence lift on craft by using
                                                     Bernoulli’s equation.
                                                 3.  Identify aircraft components; stresses during flight.
                                                 4.  Select aerospace materials for various parts of aircraft.
                                                 5.  Explain and use of aluminium and titanium alloys by heat treatment.
                                                 6.  Control microstructure of aerospace aluminium alloy by heat treatment.
                                                 7.  Apply knowledge of materials science & engineering to the fabrication
                                                     of aircraft, including riveting.
                                                 8.  Select composite materials for various parts of aircraft.
                                                 9.  Design the limited level of alloys.
                                                 10.  Apply knowledge of creep deformations at high temperature level.
                                                 11.  Relate gas-turbine design with super alloy material design.
           Transferable Skills                   None

           Synopsis of Course Contents           Theory of flight; calculation of forces; aircraft components and stresses
                                                 during flight; materials and material requirements for aerospace structures
                                                 and engines; aerospace materials selection; fabrication of aircraft structure;
                                                 polymers and composite materials; alloys for aerospace applications; gas
                                                 turbine engine design; nature, production and applications of superalloys;
                                                 turbine blade materials engineering, turbine-blade material requirements;
                                                 aerospace materials testing, production and processing; fracture, fatigue
                                                 and corrosion of aerospace materials.
           Learning Strategies (lecture, tutorial, work-  Lectures, Tutorials, AL & CL
           shop, discussion, etc)
           Assessment Weightage*                 Continuous Assessment: 60%
                                                 Final Examination:40%

           Methodologies for Feedback on Perfor-  1.  Continuous assessment before the final examination.
           mance                                 2.  Grades for final exam.

           Criteria in Summative Assessment      Refer to the University of Malaya (First Degree) Rules 2013 and the   Uni-
                                                 versity of Malaya (First Degree) Regulations 2013.


            UM-PT01-PK03-BR003(BI)-S04
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