Simulation of the heat transfer in regeneratively cooled rocket combustion chambers

被引：0

作者：

Woschnak, A ^{[1
]}

Kuhl, D ^{[1
]}

机构：

[1] Germain Aerosp Ctr, Dept Space Prop, Thermomech Modeling Grp, D-74239 Hardthausen, Germany

来源：

COMPUTATIONAL FLUID DYNAMICS '98, VOL 1, PARTS 1 AND 2 | 1998年

关键词：

D O I：

暂无

中图分类号：

O42 [声学];

学科分类号：

070206 ; 082403 ;

摘要：

This paper presents thermal fluid-structure coupling algorithms and its application to the wall structure of regeneratively cooled combustion chambers. In this analysis the finite element method is used for the simulation of the fluid flow in a cooling channel and the thermal field of the structure. The quality of the numerical fluid flow simulation is validated by means of experimental confirmed analytical results of the main engine 'Vulcain' of the European rocket 'ARIANE V'. The usefulness of the coupled thermal analysis is presented.

引用

页码：1019 / 1024

页数：6

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