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ALCOA airplane Bracket optimization

ALCOA airplane Bracket optimization

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Last crawled date: 1 year, 11 months ago

Results of the optimization:

Design material: 15-5PH per AMS5862

Elastic Modulus = 29,000 KSI = 200,000 MPa = 200 GPa

Poisson Ratio= 0.27

Yield Stress = 145 KSI = 1000 MPA

Density = 7833 kg/m^3

Results:

1250lbs X load: Maximum stress 143,3KSI

2500lbs Y load: Maximum stress 136,2KSI

1875lbs XY 45°load: Maximum stress 136,1KSI

Weight: 255g

Tags

airplane bracket alcoa optimization

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