Demiroğlu, Y. Et Al. 2021. Multi-fidelity Sonic Boom Minimization of a Supersonic Aircraft by Parametric Wing Shape Design. AIAA Scitech , (Tennessee, United States Of America), 1-20.

Demiroğlu, Y., Yıldız, Ş., & Nikbay, M., (2021). Multi-fidelity Sonic Boom Minimization of a Supersonic Aircraft by Parametric Wing Shape Design . AIAA Scitech (pp.1-20). Tennessee, United States Of America

Demiroğlu, Yusuf, Şıhmehmet Yıldız, And Melike Nikbay. "Multi-fidelity Sonic Boom Minimization of a Supersonic Aircraft by Parametric Wing Shape Design," AIAA Scitech, Tennessee, United States Of America, 2021

Demiroğlu, Yusuf Et Al. "Multi-fidelity Sonic Boom Minimization of a Supersonic Aircraft by Parametric Wing Shape Design." AIAA Scitech , Tennessee, United States Of America, pp.1-20, 2021

Demiroğlu, Y. Yıldız, Ş. And Nikbay, M. (2021) . "Multi-fidelity Sonic Boom Minimization of a Supersonic Aircraft by Parametric Wing Shape Design." AIAA Scitech , Tennessee, United States Of America, pp.1-20.

@conferencepaper{conferencepaper, author={Yusuf Demiroğlu Et Al. }, title={Multi-fidelity Sonic Boom Minimization of a Supersonic Aircraft by Parametric Wing Shape Design}, congress name={AIAA Scitech}, city={Tennessee}, country={United States Of America}, year={2021}, pages={1-20} }