Approximate method for calculating convective heat flux on the surface of bodies of simple geometric shapes

被引：19

作者：

Kuzenov, V. V. ^{[1
,2
]}

Ryzhkov, S. V. ^{[2
]}

机构：

[1] State Corp ROSATOM Co, NL Dukhov All Russian Res Inst Automat, Suschevskaya St 22, Moscow 127055, Russia

[2] Bauman Moscow State Tech Univ, 2 Baumanskaya St 5,1, Moscow 105005, Russia

来源：

10TH INTERNATIONAL CONFERENCE ON AEROPHYSICS AND PHYSICAL MECHANICS OF CLASSICAL AND QUANTUM SYSTEMS | 2017年 / 815卷

关键词：

HYPERSONIC FLOW;

D O I：

10.1088/1742-6596/815/1/012024

中图分类号：

P1 [天文学];

学科分类号：

0704 ;

摘要：

The paper formulated engineering and physical mathematical model for aerothermodynamics hypersonic flight vehicle (HFV) in laminar and turbulent boundary layers (model designed for an approximate estimate of the convective heat flow in the range of speeds M = 6-28, and height H = 20-80 km). 2D versions of calculations of convective heat flows for bodies of simple geometric forms (individual elements of the design HFV) are presented.

引用

页数：8

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