I would want to figure out the student's weakest areas, and get to know the background of the student, regarding their previous performance in various subjects, because a solution at the root level can yield enormous results in ways which can never be imagined.
I also would not prefer to have a monotonous environment so rest assure that you will not be in a regular class lecture and i will bring in real life examples from actual real time projects to keep the classes interesting
I am a mechanical engineer by under graduation and have been trained in the field of design of aero structures as per aeronautical industry standards I've also been exposed to FEM techniques, design considerations, hand calculations using approved methods, and a graduate with a Bachelor's degree in Mechanical Engineering 2018 batch, currently pursuing my masters in Mechatronics in Edith Cowan University. I've also taught my juniors subjects such as CAD and various other subjects
I've also been exposed to design of aero structures, FEM techniques, design considerations, hand calculations using approved methods and performed bolt group analysis by classical and software approach to obtain the reaction forces and stresses on the bolts
I'm also possess good level of competency on modelling tools such as Unigraphics NX, Solidworks, and solidedge which are used
i also possess good level of knowledge on metallic aircraft materials
I have been exposed to planning and developing strategies for large scale multi-disciplinary project such as Unmanned Ground Vehicles with a major focus on mechanical design. Familiar with 2D mesh, linear static analysis and buckling analysis. Exposed to implicit analysis with preprocessor such as MSC Patran and implicit solver Nastran
it depends on the level of the student and the topics which are to be covered
I currently possess a Bachelors degree in Mechanical engineering and am pursuing my masters in mechatronics engineering in Edith Cowen University. I have also worked on a few projects such as design of Shear fitting for an Aircraft vertical tail stabiliser as per ESDU 91008 ,analysis of secondary brackets, and also sizing od skin stringer panels,
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