INTRODUCTION TO AIRCRAFT INTERIORS - STOWAGE UNIT STRESS ANALYSIS

The student will obtain hands on experience of running the interface load Finite Element Model (FEA) in Nastran and acquire stress and deflection data. They will stress analyse in MathCad (or similar), the major composite and metallic parts using the loadcase data. It is important that the student first attends the Interface Loads Derivation course to fully appreciate this Stress Analysis course.