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.
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页数：6
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