Propagation of the Wave Packet in a Boundary Layer of Swept Wing at Mach Number 2

被引：0

作者：

Yermolaev, Yury G. ^{[1
]}

Yatskikh, Aleksey A. ^{[1
,2
]}

Kosinov, Alexander D. ^{[1
,2
]}

Semionov, Nickolay V. ^{[1
]}

机构：

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

[2] Novosibirsk State Univ, Pirogova Str 2, Novosibirsk 630090, Russia

来源：

PROCEEDINGS OF THE XXV CONFERENCE ON HIGH-ENERGY PROCESSES IN CONDENSED MATTER (HEPCM 2017) | 2017年 / 1893卷

关键词：

STABILITY;

D O I：

10.1063/1.5007445

中图分类号：

O59 [应用物理学];

学科分类号：

摘要：

The evolution of the artificial wave packet in the supersonic boundary layer of swept wing was experimentally studied for the first time by hot-wire measurements. The localized disturbances were generated by pulse glow discharge. Analysis of the mean flow, integral dependences, and the averaged waveforms of wave packet in supersonic boundary layer of swept wing has been executed.

引用

页数：7

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