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平流层飞艇强迫对流特性数值仿真分析

武江涛 麻震宇 侯中喜 柳兆伟

国防科技大学学报2016,Vol.38Issue(2):177-182,6.
国防科技大学学报2016,Vol.38Issue(2):177-182,6.DOI:10.11887/j.cn.201602029

平流层飞艇强迫对流特性数值仿真分析

Numerical research on forced convective heat transfer of stratospheric airships

武江涛 1麻震宇 1侯中喜 1柳兆伟1

作者信息

  • 1. 国防科技大学 航天科学与工程学院,湖南 长沙410073
  • 折叠

摘要

Abstract

During the floating flight,the complex radiation-convection environment remarkably affects the flight performance and security of the stratospheric airship.The forced convection around the stratospheric airship plays an important role in the thermal behavior of the airship.Based on the hypothesis of pure heat conduction inside the airship,a three dimensional CFD model of stratospheric airships was developed and the thermal characteristics of the forced convective heat transfer of the airship were investigated.The distributions of the temperature of skins of the airship and the average temperature of the inner gas were calculated with the variation of the angle of the sun,the wind velocity and the angle of attack. Simulation results can be referenced for the accurate prediction of the thermal behavior of stratospheric airships.

关键词

平流层飞艇/强迫对流/计算流体力学/数值仿真

Key words

stratospheric airships/forced convection/computational fluid dynamics/numerical simulation

分类

航空航天

引用本文复制引用

武江涛,麻震宇,侯中喜,柳兆伟..平流层飞艇强迫对流特性数值仿真分析[J].国防科技大学学报,2016,38(2):177-182,6.

基金项目

国家高分辨率对地观测系统重大专项支持项目 ()

国防科技大学学报

OA北大核心CSCDCSTPCD

1001-2486

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