Heat transfer and behavior of ultra high temperature ceramic materials under exposure to supersonic carbon dioxide plasma with additional laser irradiation

被引:2
作者
Chaplygin, A. [1 ]
Simonenko, E. [2 ]
Simonenko, N. [2 ]
Kotov, M. [1 ]
Yakimov, M. [1 ]
Lukomskii, I. [1 ]
Galkin, S. [1 ]
Kolesnikov, A. [1 ]
Vasil'evskii, S. [1 ]
Shemyakin, A. [1 ]
Solovyov, N. [1 ]
机构
[1] RAS, Ishlinsky Inst Problems Mech, Prospekt Vernadskogo 101-1, Moscow 119526, Russia
[2] RAS, Kurnakov Inst Gen & Inorgan Chem, Leninsky Pr 31, Moscow 119991, Russia
基金
俄罗斯科学基金会;
关键词
Induction plasmatron; Carbon dioxide; Laser; Heat transfer; Combined heating; Ceramics; DISSOCIATED AIR; CATALYTIC RECOMBINATION; ZRB2-SIC CERAMICS; SURFACE; FLOW; COMPOSITES; EMISSIVITY; OXIDATION; GRAPHITE; PROPERTY;
D O I
10.1016/j.ijthermalsci.2024.109005
中图分类号
O414.1 [热力学];
学科分类号
摘要
The behavior of the ultra high temperature ceramic material HfB2-SiC-C(graphene) under exposure to a supersonic carbon dioxide plasma, with and without the addition of laser irradiation, has been studied. The material was heated to 1750 degrees C in an inductively coupled plasma jet without laser irradiation. A temperature jump to 2190 degrees C was observed when additional ytterbium laser irradiation was applied to the surface. The spectral emissivity of the heated surface at wavelengths of 0.65 and 0.9 mu m was studied. It was found that the spectral emissivity decreases as the material oxidizes. The heat flux to the surface of the heated material was measured and compared to the heat flux to a cold copper surface under the same conditions. Analysis of the surface of HfB2-SiC-C(graphene) material after exposure was performed. Differences in microstructure were detected between specimens exposed to carbon dioxide plasma with and without additional laser irradiation.
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页数:11
相关论文
共 75 条
[1]   Co-reinforcing of ZrB2-SiC ceramics with optimized ZrC to Cf ratio [J].
Adibpur, Farhad ;
Tayebifard, Seyed Ali ;
Zakeri, Mohammad ;
Asl, Mehdi Shahedi .
CERAMICS INTERNATIONAL, 2020, 46 (14) :22661-22673
[2]   Flow and Heat Transfer in Underexpanded Air Jets Issuing from the Sonic Nozzle of a Plasma Generator [J].
Afonina, N. E. ;
Vasil'evskii, S. A. ;
Gromov, V. G. ;
Kolesnikov, A. F. ;
Pershin, I. S. ;
Sakharov, V. I. ;
Yakushin, M. I. .
FLUID DYNAMICS, 2002, 37 (05) :803-814
[3]   Emissivity and catalycity measurements on SiC-coated carbon fibre reinforced silicon carbide composite [J].
Alfano, Davide ;
Scatteia, Luigi ;
Cantoni, Stefania ;
Balat-Pichelin, Marianne .
JOURNAL OF THE EUROPEAN CERAMIC SOCIETY, 2009, 29 (10) :2045-2051
[4]   HYPERSONIC WAVERIDERS FOR PLANETARY-ATMOSPHERES [J].
ANDERSON, JD ;
LEWIS, MJ ;
KOTHARI, AP ;
CORDA, S .
JOURNAL OF SPACECRAFT AND ROCKETS, 1991, 28 (04) :401-410
[5]   Aerogravity-assist maneuvers: Coupled trajectory and vehicle shape optimization [J].
Armellin, Roberto ;
Lavagna, Michele ;
Starkey, Ryan P. ;
Lewis, Mark J. .
JOURNAL OF SPACECRAFT AND ROCKETS, 2007, 44 (05) :1051-1059
[6]   Influence of graphite nano-flakes on densification and mechanical properties of hot-pressed ZrB2-SiC composite [J].
Asl, Mehdi Shahedi ;
Kakroudi, Mandi Ghassemi ;
Kondolaji, Rouhollah Abedi ;
Nasiri, Hadi .
CERAMICS INTERNATIONAL, 2015, 41 (04) :5843-5851
[7]   Emissivity, catalycity and microstructural characterization of ZrB2-SiCfiber based UHTC at high temperature in a non-equilibrium air plasma flow [J].
Balat-Pichelin, M. ;
Beche, E. ;
Sciti, D. ;
Alfano, D. .
CERAMICS INTERNATIONAL, 2014, 40 (07) :9731-9742
[8]   Emissivity measurements of opaque gray bodies up to 2000 °C by a dual-frequency pyrometer [J].
Biasetto, L. ;
Manzolaro, M. ;
Andrighetto, A. .
EUROPEAN PHYSICAL JOURNAL A, 2008, 38 (02) :167-171
[9]  
Bugel M., 2011, Int. J. Aerosp. Eng., V2011
[10]   Heat transfer in ultra-high temperature advanced ceramics under high enthalpy arc-jet conditions [J].
Cecere, Anselmo ;
Savino, Raffaele ;
Allouis, Christophe ;
Monteverde, Frederic .
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2015, 91 :747-755