Heat transfer in supersonic separated flow of the compression corner

被引：0

作者：

Zapryagaev, V., I ^{[1
]}

Kavun, I. N. ^{[1
]}

Trubitsyna, L. P. ^{[1
]}

机构：

[1] Khristianovich Inst Theoret & Appl Mech, Novosibirsk 630090, Russia

来源：

XXXV SIBERIAN THERMOPHYSICAL SEMINAR, 2019 | 2019年 / 1382卷

关键词：

D O I：

10.1088/1742-6596/1382/1/012049

中图分类号：

O414.1 [热力学];

学科分类号：

摘要：

This article presents the study results for heat transfer in supersonic laminar separated compression corner flow. The study was carried out for free-stream Mach number M = 6 and the compression ramp angle in the range of phi = 20 degrees - 40 degrees.

引用

页数：6

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