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介绍了现有的应用于航天领域的电弧加热设备类型,包括叠片、管弧或涡稳、磁稳、感应以及磁等离子动力加热器.描述了主要的设备,同时对电弧加热设备的发展趋势进行了介绍.

The types of operational aerospace arc heater facility is performed. These facility include multi-seg- ment, huels or vortex stabilized, magnetically-stabilized, induction-coupled and magnetplasmdynamic heaters. The main facility is described. The trend of arc heater facility is also introduced in this paper.

参考文献

[1] Amundson M H;Smith D M .Ground test and evaluation methodologies and techniques for the development of endoatmospheric interceptors AIAA Paper 93-2679[R].,1993.
[2] Smith R K;Wagner D A .A survey of current and future plasma arc-heated test facilities for aerospace and commercial applications AIAA Paper 98-0146[R].,1998.
[3] Mark P L .Arc-jet semi-elliptic nozzle simulations and validation in support of X-33 TPS testing AIAA Paper 98-0864[R].,1998.
[4] Jay H G;David A S;Charles A S .High enthalpy test methodologies for thermal protection systems development at NASA Ames research center AIAA Paper,2005-3326[R].
[5] Ernest F F .NASA AMES arc jets and range capabilities for planetary entry NASA 2007001463[R].,2007.
[6] Boyd Jack .NASA Ames research center overview NASA 2007008268[R].,2007.
[7] Rochelle W C;Battley H H .Orbiter TPS development and certification testing at the NASA/JSC 10 MW atmospheric reentry materials and structures evaluation facility AIAA Paper 83-0147[R].,1983.
[8] Max E L;Jeremiah J M .Boundary layer transition protuberance tests at NASA JSC arc-jet facility AIAA Paper AIAA Paper 2010-1578[R].,2010.
[9] Thomas S R;Voland R T;Guy R W .Test flow calibration study of the Langley arc-heated acramjet test facility AIAA Paper 87-2165[R].,1987.
[10] Guy R W;Rogers R C;Puster R L et al.The NASA Langley scramjet test complex AIAA Paper 96-3243[R].,1996.
[11] Karen F C;Kenneth E R .A finite rate chemical analysis of nitric oxide flow contamination effects on scramjet performance NASA/TP-2003-2 12159[R].,2003.
[12] David W W;Richard G I;Aaron H A et al.1998calibration of the Mach 4.7 and Mach 6 arc-heated scramjet test facility nozzles NASA/TM-2004-213250[R].,2004.
[13] Bruce W E;Horn D D;Felderman E J et al.Arc heater development at AEDC AIAA Paper 94-2591[R].,1994.
[14] Felderman E J;Chapman R;Jacocks J L .Development of a high-pressure,high-power arc heater:modeling requirements and status AIAA Paper 94-2658[R].,1994.
[15] Smith D M;Younker Lt T .Comparative ablation testing of carbon phenolic TPS materials in the AEDC-H1 arcjet AIAA Paper 2005-3263[R].,2005.
[16] Antonio Del Vecehio;Federico De Filippis .Scirocco plasma wind tunnel:low enthalpy by use of cold Air transverse injection AIAA Paper 2003-6959[R].,2003.
[17] Caristia S;De Filippis F;Del Vecchio A.Scirocco PWT facility for high temperature resistant material assembies test[A].Bremen,Germany,2003
[18] Antonio D V;Gennaro C .IR thermographic measurements of temperatures in hypersonic large-scale plasma flow AIAA Paper 2003-6926[R].,2003.
[19] Anfimov N .TsNIIMASH capabilities for aerogasdynamical and thermal testing of hypersonic vehicle AIAA Paper 92-3962[R].,1992.
[20] Terranee M D .Development of a mid-pressure archeated facility for hypersonic vehicle testing AIAA Paper 2010-1732[R].,2010.
[21] Montgomery P;Smith D M;Sheeley J et al.The quest for total pressures:justification and current development efforts for a higher pressure arc heater facility AIAA Paper 2004-6815[R].,2004.
[22] Sheeley J;Whittingham K;Montgomery P et al.Extending arc heater operatingpressure range for improved reentry simulation AIAA Paper 2006-3295[R].,2006.
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