NUMERICAL SIMULATION OF FLOW AND HEAT TRANSFER IN THE BASE REGION OF MARTIAN DESCENT VEHICLE

被引：0

作者：

Egorov, Ivan ^{[1
]}

机构：

[1] Cent Aerohydrodynam Inst TsAGI, Zhukovskii, Moscow Region, Russia

来源：

PROCEEDINGS OF THE ASME INTERNATIONAL HEAT TRANSFER CONFERENCE - 2010, VOL 1: BIO HEAT TRANSFER, BOILING HEAT TRANSFER, COMPUTATIONAL HEAT TRANSFER | 2010年

关键词：

D O I：

暂无

中图分类号：

Q6 [生物物理学];

学科分类号：

071011 ;

摘要：

Numerical investigation of hypersonic flow and heating over two models of an interplanetary probe was carried out at Mach numbers from 6 to 20 and Reynolds numbers Re,, D from 0.7x10(5) to 16x10(5). The models differ mainly by the shape of the back surface simulating the payload container. The Reynolds number, at which laminar-turbulent transition takes place in the near wake, was defined at Mach numbers M =6-8. It was shown that at turbulent base flow, the heat flux to the back surface of a blunted body can be comparable with the heat flux at the forward stagnation point. The results of numerical flow within the framework of Navier-Stokes and Reynolds equations simulation were compared with the experimental data.

引用

页码：915 / 923

页数：9

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