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Numerical Analysis of Effect of Boundary Layer Characteristics on the Flow Field in S-shaped Inlet

In order to explore the effect of boundary layer thickness and pressure gradient on the performance of the flow field in the inlet, we design a high offset rate S-shaped inlet based on a certain unmanned aerial vehicle (UAV), and its author has analyzed the effect of boundary layer characteristics o...

Бүрэн тодорхойлолт

-д хадгалсан:
Номзүйн дэлгэрэнгүй
Үндсэн зохиолчид: Ren Jia, Wu Naiming, Li Mingzhen, Hu Qiyang, Liu He
Формат: Artigo
Хэл сонгох:Inglês
Хэвлэсэн: EDP Sciences 2015-01-01
Цуврал:MATEC Web of Conferences
Нөхцлүүд:
Онлайн хандалт:http://dx.doi.org/10.1051/matecconf/20152501011
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