Application Area of Fundamental Knowledge about the Flow Around a Wing at Low Reynolds Numbers

被引：0

作者：

Zanin, Boris ^{[1
]}

Kozlov, Victor ^{[1
]}

Zverkov, Ilya ^{[1
,2
]}

Kryukov, Alexey ^{[1
,2
]}

机构：

[1] Khristianovich Inst Theoret & Appl Mech SB RAS, Inst Skaya Str 4-1, Novosibirsk 630090, Russia

[2] Novosibirsk State Tech Univ, Karl Marks Str 20, Novosibirsk 630073, Russia

来源：

HIGH-ENERGY PROCESSES IN CONDENSED MATTER (HEPCM 2020) | 2020年 / 2288卷

关键词：

D O I：

10.1063/5.0028775

中图分类号：

O59 [应用物理学];

学科分类号：

摘要：

The work is devoted to the review of aircraft that are operated or are in the design stage, whose wings or blades streamline under the condition of low Reynolds numbers. By low Reynolds numbers, it is meant that this number taken along the chord of the aircraft wing at a cruising flight speed is less than Re = 500 000. It is under these flow conditions in the wing boundary layer that specific separation zones appear, the modification of which with the help of an wavy surface of the wing can bring about an improvement in aerodynamic characteristics of the aircraft as a whole.

引用

页数：8

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