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.)
Experimental evaluation and numerical simulation of performance of the bypass dual throat nozzle
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering ( IF 1.0 ) Pub Date : 2020-09-21 , DOI: 10.1177/0954410020959886 Mohammad Hadi Hamedi-Estakhrsar 1 , Hossein Mahdavy-Moghaddam 1
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering ( IF 1.0 ) Pub Date : 2020-09-21 , DOI: 10.1177/0954410020959886 Mohammad Hadi Hamedi-Estakhrsar 1 , Hossein Mahdavy-Moghaddam 1
Affiliation
Bypass dual throat nozzle (BDTN) is a modern concept of fluidic thrust vector control. This method able to solve the problem of thrust loss without need the secondary mass flow from other part of e...
中文翻译：
旁通双喉喷嘴性能的实验评价与数值模拟
旁路双喉喷嘴 (BDTN) 是流体推力矢量控制的现代概念。这种方法可以解决推力损失的问题，而无需从其他部分的二次质量流...
更新日期：2020-09-21
中文翻译：
旁通双喉喷嘴性能的实验评价与数值模拟
旁路双喉喷嘴 (BDTN) 是流体推力矢量控制的现代概念。这种方法可以解决推力损失的问题，而无需从其他部分的二次质量流...
京公网安备 11010802027423号