Effects of stability margin and thrust specific fuel consumption constrains on multi-disciplinary optimization for blended-wing-body design

Autor: ZHANG, Minghui, CHEN, Zhenli, TAN, Zhaoguang, GU, Wenting, LI, Dong, YUAN, Changsheng, ZHANG, Binqian
Zdroj: In Chinese Journal of Aeronautics August 2019 32(8):1847-1859
Databáze: ScienceDirect