I am doing a topology optimization on a Aircraft wing-fuselage lug. And it also optimize the component without any error in its '.out' file. But when I check the results in Hyperview of its last 20th iteration, it is completely removing my design space material. So should I take the resulted component from 9th or 10th iterative solution or Is it because the stress induced is very less than the max stress constraint applied or I'm doing any thing wrong? Please anyone guide me.
Thankyou