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This course introduces how to handle stress, stability analysis in the design of aerospace engineering components, solving problems in mechanics by using computers. Learning by their own, problems of the application and professionalism will be discussed in this course. Throughout the course, the students will be mature enough to operate and analyze aerospace engineering components subject to different types of loading individually.


This course does not involve any written exams. Students need to answer 5 assignment questions to complete the course, the answers will be in the form of written work in pdf or word. Students can write the answers in their own time. Each answer needs to be 200 words (1 Page). Once the answers are submitted, the tutor will check and assess the work.


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Course Credit: Middle East Technical University

Course Curriculum

Module: 01
Introduction and free body diagrams 00:10:00
Forces and stresses 00:10:00
Stress transformation and Mohr’s circle 00:15:00
Stress equilibrium equations 00:10:00
Module: 02
Strain and index notation 00:15:00
Strain compabitibility; strain-displacement relations 00:10:00
Generalized Hooke’s Law 00:15:00
2-D plane elasticity problems 00:15:00
Airy Stress function 00:12:00
Module: 03
2-D elasticity problems in polar coordinates 00:10:00
Stress based failure theories and fracture theory 00:16:00
Fracture mechanics 00:07:00
Elastic instability and buckling-note 00:10:00
Elastic instability and buckling-examples 00:07:00
Module: 04
Torsion for axisymmetric bodies-note 00:10:00
Torsion for axisymmetric bodies-note 2 00:16:00
Prandtls stress function 00:12:00
Lecture cylinders 00:10:00
norton_example 00:05:00
Submit Your Assignment 00:00:00
Certification 00:00:00

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