全部 标题 作者
关键词 摘要

OALib Journal期刊
ISSN: 2333-9721
费用:99美元

查看量下载量

相关文章

更多...

高温绝热毡有效热导率的理论分析与实验研究

Full-Text   Cite this paper   Add to My Lib

Abstract:

?建立了高温绝热毡有效热导率的数值计算模型,分析了温度和压力对传热机制的影响.用高真空平板型石墨加热炉测量了纤维绝热毡平均温度高达860℃时的有效热导率,实验结果与理论计算吻合得很好.结果表明,当温度较低(<400℃)时,高温隔热毡的固体传导在总体传热中占主导地位;当温度较高时(>700℃),无论环境压力高低,辐射都成为材料内部主导的传热方式;当环境压力小于200pa时,可忽略气体传导的影响.

References

[1]  1m.l.blosser,r.r.chen,i.h.schmidt,aiaa2002-0504(2002)
[2]  2j.d.verschoor,p.greebler,n.j.manville,journalofheattransfer,74,961(1952)
[3]  3j.marschall,aiaa2001-2822(2001)
[4]  4s.d.williams,d.m.curry,predictionofrigidsilicabasedinsulationconductivityusingmorphologicaldata,americansocietyofmechanicalengineers,heattransferdivision,(publication)htd,atlanta,georgia,usa,publbyasme,newyork,ny,usa,249,51(1993)
[5]  5t.w.tong,q.s.yang,c.l.tien,journalofheattransfer,43(81),(1981)
[6]  6c.f.matt,m.e.cruz,aiaa2001-2968(2001)
[7]  7s.c.lee,g.r.cunnington,journalofthermophysicsandheattransfer,44(2),121(2000)
[8]  8kamrandaryabeigi,designofhightemperaturemultilayerinsulationforreusablelaunchvehicles,ph.d.dissertation,universityofvirginia,charlottesville,va,(2000)
[9]  10kamrandaryabeigi,aiaa99-1044(1999)
[10]  11kamrandaryabeigi,aerodynamicheating,alaa2001-2834(2001)
[11]  12kamrandaryabeigi,aiaa2002-3332(2002)
[12]  9kamrandaryabeigi,effectivethermalconductivityofhightemperatureinsulationsforreusablelaunchvehicles.nasa/tm-1999-208972,(1999)
[13]  13mazhonghui,sunqin,journalofastronautics,24(5),543(2003)(马忠辉,孙秦,宇航学报,24(5),543(2003))
[14]  14baidan,fanxuji,journalofnanjinguniversityofaeronautics&astronautics,37(4),403(2005)(白丹,范绪箕,南京航空航天大学学报,37(4),403(2005))
[15]  15xieweihua,zhangboming,dushanyi,actaaeronautieaetastronauticasinica,27(4),650(2006)(解维华,张博明,杜善义,航空学报,27(4),650(2006))
[16]  16c.c.poteet,h.a.khajeel,s.y.hsu,aiaa2002-0505(2002)
[17]  17kamrandaryabeigi,j.r.knutson,j.g.sikora,nasa/tm-2002-211734(2002)

Full-Text

Contact Us

service@oalib.com

QQ:3279437679

WhatsApp +8615387084133