Oxidation Behavior of Aerospace Materials in High Enthalpy Flows Using an Oxyacetylene Torch Facility

被引:54
作者
Miller-Oana, Melia [1 ]
Neff, Paul [1 ]
Valdez, Mario [1 ]
Powell, Amber [1 ]
Packard, Matthew [1 ]
Walker, Luke S. [1 ]
Corral, Erica L. [1 ]
机构
[1] Univ Arizona, Dept Mat Sci & Engn, Arizona Mat Lab, Tucson, AZ 85721 USA
基金
美国国家科学基金会;
关键词
TEMPERATURE CERAMIC COMPOSITES; INDUCED IODINE FLUORESCENCE; CARBON-CARBON COMPOSITES; ABLATION RESISTANCE; CARBON/CARBON COMPOSITES; THERMAL-CONDUCTIVITY; ZRB2-SIC CERAMICS; CARBIDE; FLAME;
D O I
10.1111/jace.13462
中图分类号
TQ174 [陶瓷工业]; TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
The oxyacetylene torch facility is used to measure the ablation rates of graphite and the surface temperatures of different aerospace materials. The free-stream flame environment is characterized as a function of flame chemistry for heat flux, pO(2), and flow velocity. Measured ablation rates for graphite increase as a function of increasing heat flux and pO(2), which are validated by applying an oxygen diffusion based model. The model uses experimentally measured values for temperature, pO(2), and gas velocity in order to confirm torch testing results are reliable and reproducible. Surface temperatures of ultra-high temperature ceramic composites are measured as a function of increasing heat flux and show an enthalpic cooling effect on the flame during oxidation testing.
引用
收藏
页码:1300 / 1307
页数:8
相关论文
共 45 条
[1]   SPECTRAL EMISSIVITY MEASUREMENTS OF ABLATING PHENOLIC GRAPHITE [J].
CHANG, JH ;
SUTTON, GW .
AIAA JOURNAL, 1969, 7 (06) :1110-&
[2]  
Chase M., 1998, NIST-JANAF Thermochemical Tables, V1
[3]   Microstructure and evolution of iridium coating on the C/C composites ablated by oxyacetylene torch [J].
Chen, Zhaofeng ;
Wu, Wangping ;
Cheng, Han ;
Liu, Yong ;
Wang, Shiming ;
Xue, Ruijuan .
ACTA ASTRONAUTICA, 2010, 66 (5-6) :682-687
[4]   Ultra-high-temperature ceramic coatings for oxidation protection of carbon-carbon composites [J].
Corral, Erica L. ;
Loehman, Ronald E. .
JOURNAL OF THE AMERICAN CERAMIC SOCIETY, 2008, 91 (05) :1495-1502
[5]   Improved ablation resistance of C-C composites using zirconium diboride and boron carbide [J].
Corral, Erica L. ;
Walker, Luke S. .
JOURNAL OF THE EUROPEAN CERAMIC SOCIETY, 2010, 30 (11) :2357-2364
[6]   THE MELTING POINT-COMPOSITION DIAGRAM OF THE ZIRCONIUM-OXYGEN SYSTEM [J].
CUBICCIOTTI, D .
JOURNAL OF THE AMERICAN CHEMICAL SOCIETY, 1951, 73 (05) :2032-2035
[7]   OXIDATION-RESISTANT CARBON-CARBON COMPOSITES UP TO 1700-DEGREES-C [J].
DHAMI, TL ;
BAHL, OP ;
AWASTHY, BR .
CARBON, 1995, 33 (04) :479-490
[8]  
Esser B, 1999, ESA SP PUBL, V420, P545
[9]   Thermodynamic analysis of ZrB2-SiC oxidation:: Formation of a SiC-depleted region [J].
Fahrenholtz, William G. .
JOURNAL OF THE AMERICAN CERAMIC SOCIETY, 2007, 90 (01) :143-148
[10]   Morphology and microstructure of 2.5 dimension C/SiC composites ablated by oxyacetylene torch [J].
Fang, Dan ;
Chen, Zhaofeng ;
Song, Yingdong ;
Sun, Zhigang .
CERAMICS INTERNATIONAL, 2009, 35 (03) :1249-1253