Experimental Study of the Heat Transfer at Compressible Gas Flow with a Favorable Pressure Gradient

被引：1

作者：

Kiselev, N. A. ^{[1
]}

Malastovskii, N. S. ^{[1
,2
]}

Zditovets, A. G. ^{[1
]}

Vinogradov, Yu. A. ^{[1
]}

机构：

[1] Moscow MV Lomonosov State Univ, Inst Mech, Moscow, Russia

[2] Bauman Moscow State Tech Univ, Moscow 107005, Russia

来源：

HIGH TEMPERATURE | 2023年 / 61卷 / 04期

基金：

俄罗斯科学基金会;

关键词：

TURBULENT-BOUNDARY-LAYER; TRANSITION;

D O I：

10.1134/S0018151X23040065

中图分类号：

O59 [应用物理学];

学科分类号：

摘要：

The parameters of heat transfer at compressible gas flow with a favorable pressure gradient have been experimentally studied. The heat transfer coefficients and the temperature of thermally insulated (adiabatic) wall are determined using the transient heat transfer method. To estimate the degree of flow laminarization, the results obtained are compared with the known dependences for the turbulent boundary layer developing on a plate in a zero-pressure gradient flow. Some regularities of the effect of flow acceleration on the heat transfer law are revealed for the studied configurations of supersonic nozzles.

引用

页码：535 / 543

页数：9

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[1] Experimental Study of the Heat Transfer at Compressible Gas Flow with a Favorable Pressure Gradient
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N. S. Malastovskii
A. G. Zditovets
Yu. A. Vinogradov
[J]. High Temperature, 2023, 61 : 535 - 543
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