I have derived the relationship between an arbitrary compressive strain-stress diagram and critical buckling stress for the console of a given slendernes 'lamda'. Now I need to verify the plots received 'sigma'('lamda') for an alloy Al 7075 T6 or the composites Al-Si3N4, Al-Al2O3. Unfortunately, i didn't find in literature the experimental data for global buckling but only for local on in the case of thin-walled structures (TWS). And these stresses are many times less.

Thank You in advance for this data especial for the beams of standard sections: L-,I-,H- etc but not TWS.

Best regards Viktor

More Viktor Vladimir Chistyakov's questions See All
Similar questions and discussions