主要论述长时间气动加热飞行器热防护系统隔热机理的新概念,提出传统的单相固体热传导由于其隔热机制的局限性,已不能解决新型高超声速式飞行器的隔热问题,代之以气-固的辐射-传导-对流复合传热机制.多相复合传热机理可解决长时间气动加热飞行器隔热的问题.
参考文献
| [1] | Kamran Dergabeigs .Thermal analysis and design of multi-layer insulation for re-entry aerodynamic heating[J].AIAA Journal,2001,2:834. |
| [2] | Kamvan Darjabcig .Heat transfer in high temperature fibrous insulation[J].AIAA Journal,2002,3:332. |
| [3] | Marschall J et al.Internal radiation transport and effective thermal consluctivily of fibrous ceramic insulation[J].AIAA Journal,2001,2:822. |
| [4] | Petrov V A .Combined radiation and conduction heat transfer in high temperature fiber thermal insulation[J].International Journal of Heat and Mass Transfer,1997,40(09):2241-2247. |
| [5] | Imakoma H;Sang K;Okazard U .The effective thermal conductivity of fibrous insulation[J].International Chemical Engineering,1990,36:738-746. |
上一张
下一张
上一张
下一张
计量
- 下载量()
- 访问量()
文章评分
- 您的评分：
-
10%
-
20%
-
30%
-
40%
-
50%