当前位置：
X-MOL 学术
›
Proc. Inst. Mech. Eng. Part G J. Aerosp. Eng.
›
论文详情
Our official English website, www.x-mol.net, welcomes your
feedback! (Note: you will need to create a separate account there.)
Numerical multidisciplinary optimization of aircraft with flight dynamic stability constraints
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering ( IF 1.0 ) Pub Date : 2020-06-01 , DOI: 10.1177/0954410020926659 Jacek Mieloszyk 1
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering ( IF 1.0 ) Pub Date : 2020-06-01 , DOI: 10.1177/0954410020926659 Jacek Mieloszyk 1
Affiliation
Classical approach to conceptual and preliminary design in aerospace sciences reaches limits. To go further and achieve better, competitive results’ use of optimization methods becomes mandatory. T...
中文翻译：
具有飞行动力稳定性约束的飞机多学科数值优化
航空航天科学中概念和初步设计的经典方法达到了极限。为了走得更远并取得更好的成绩，竞争结果必须使用优化方法。天...
更新日期：2020-06-01
中文翻译：
具有飞行动力稳定性约束的飞机多学科数值优化
航空航天科学中概念和初步设计的经典方法达到了极限。为了走得更远并取得更好的成绩，竞争结果必须使用优化方法。天...
京公网安备 11010802027423号