ALCOA airplane Bracket optimization
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The optimization results indicate that the design material used is 15-5PH as per AMS5862. It has an elastic modulus of 29,000 KSI (or 200,000 MPa or 200 GPa), a Poisson ratio of 0.27, and a yield stress of 145 KSI (or 1000 MPa). The material density is 7833 kg/m³. Load tests revealed that with a 1250lbs X load, the maximum stress was 143,3KSI; a 2500lbs Y load resulted in a maximum stress of 136,2KSI; and a 1875lbs XY 45°load led to a maximum stress of 136,1KSI. The weight of the final product is 255g.
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