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Examine point load (500 N to 5000 N in increments of 500 N) at the wing tip using Aluminium Alloy (AA2024). Justify your answers. b) Compare these results with theoretical solutions. Material Comparison: Analyze the effects of Aluminium, Titanium, Steel, and Carbon Fiber for a velocity range of 40 m/s to 90 m/s in 10 m/s increments. Justify your material choice.

Part A: Practical Session Attend Practical Session: Obtain results from the laboratory session. Activities and findings introduced by the tutor […]

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