导弹与航天运载技术
導彈與航天運載技術
도탄여항천운재기술
MISSILES AND SPACE VEHICLES
2015年
1期
88-91
,共4页
李亚男%刘鑫%刘佳琪%王明亮%贺志宏
李亞男%劉鑫%劉佳琪%王明亮%賀誌宏
리아남%류흠%류가기%왕명량%하지굉
蜂窝%发射率%仿真
蜂窩%髮射率%倣真
봉와%발사솔%방진
Honeycomb%Emissivity%Simulation
基于蒙特卡罗法(MCM)建立蜂窝结构瞬态传热仿真模型,进行了蜂窝结构隔热性能的数值模拟,重点研究蜂窝腔内不同表面发射率对其传热性能的影响。研究结果表明,在空间低温环境条件下,通过减小蜂窝腔内表面平均发射率可以使蜂窝结构材料具有更好的隔热性能,其中,蜂窝腔内顶面、底面发射率对蜂窝隔热性能的影响大于侧面发射率的影响。
基于矇特卡囉法(MCM)建立蜂窩結構瞬態傳熱倣真模型,進行瞭蜂窩結構隔熱性能的數值模擬,重點研究蜂窩腔內不同錶麵髮射率對其傳熱性能的影響。研究結果錶明,在空間低溫環境條件下,通過減小蜂窩腔內錶麵平均髮射率可以使蜂窩結構材料具有更好的隔熱性能,其中,蜂窩腔內頂麵、底麵髮射率對蜂窩隔熱性能的影響大于側麵髮射率的影響。
기우몽특잡라법(MCM)건립봉와결구순태전열방진모형,진행료봉와결구격열성능적수치모의,중점연구봉와강내불동표면발사솔대기전열성능적영향。연구결과표명,재공간저온배경조건하,통과감소봉와강내표면평균발사솔가이사봉와결구재료구유경호적격열성능,기중,봉와강내정면、저면발사솔대봉와격열성능적영향대우측면발사솔적영향。
Heat transfer and temperature distribution in honeycomb composites during transient condition were investigated by means of numerical simulations based on Monte Carlo Method. Infrared (IR) radiation in honeycomb core cells was particularly studied and analyzed in this paper in order to find out the effect of emissivity (or size) on heat transfer. The results show that thermal conductivity of honeycomb will be effectively enhanced when emissivity (or thickness) in honeycomb core cells increases. And the effect of top-surface emissivity and under-surface emissivity in honeycomb core cells is more evident than that of side-face emissivity.