ZrB2-SiC Sharp Leading Edges in High Enthalpy Supersonic Flows
Author:
Affiliation:
1. National Research Council of Italy; Institute of Science and Technology for Ceramics; Via Granarolo 64 48018 Faenza Italy
2. Department of Aerospace Engineering; University of Naples “Federico II,”; P.le Tecchio 80 80125 Naples Italy
Publisher
Wiley
Subject
Materials Chemistry,Ceramics and Composites
Link
http://onlinelibrary.wiley.com/wol1/doi/10.1111/j.1551-2916.2012.05226.x/fullpdf
Reference45 articles.
1. Material Property Requirements for Analysis and Design of UHTC Components in Hypersonic Applications;Squire;J. Eur. Ceram. Soc.,2010
2. UHTC Composites for Hypersonic Applications;Paul;Am. Ceram. Soc. Bull.,2012
3. Thermal Conductivity Characterization of Hafnium Diboride-Dased Ultra-High-Temperature Ceramics;Gasch;J. Am. Ceram. Soc.,2008
4. Thermal and Electrical Transport Properties of Spark Plasma-Sintered HfB2 and ZrB2 Ceramics;Zhang;J. Am. Ceram. Soc.,2011
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