Design of shape morphing hypersonic inward-turning inlet using multistage optimization
J Wang, J Cai, Y Duan, Y Tian - Aerospace Science and Technology, 2017 - Elsevier
To make a compromise between compression efficiency and aerodynamic performance, a
novel multistage optimization approach is proposed to improve the design of the shape …
novel multistage optimization approach is proposed to improve the design of the shape …
[HTML][HTML] Aerodynamic configuration integration design of hypersonic cruise aircraft with inward-turning inlets
W Jifei, CAI Jinsheng, LIU Chuanzhen, D Yanhui… - Chinese Journal of …, 2017 - Elsevier
In this work, a novel airframe/propulsion integration design method of the wing-body
configuration for hypersonic cruise aircraft is proposed, where the configuration is integrated …
configuration for hypersonic cruise aircraft is proposed, where the configuration is integrated …
[HTML][HTML] 三维超声速流动的压力反问题
蓝庆生， 赵玉新， 赵一龙， 刘红阳 - 2017 - html.rhhz.net
为了进一步探索三维超声速流道的设计方法, 采用一种预设壁面压力分布计算壁面型线的思想,
并结合双特征线方法提出一种全三维超声速流动压力反问题的求解方法. 在三维超声速流场设计 …
并结合双特征线方法提出一种全三维超声速流动压力反问题的求解方法. 在三维超声速流场设计 …