1. Experimental Investigation of Cermet Turbine Blades in an Axial-Flow Turbojet Engine, NASA Technical Report;Morgan,1957
2. Near net-shape, ultra-high melting, recession-resistant ZrC/W-based rocket nozzle liners via the displacive compensation of porosity (DCP) method;Dickerson;J. Mater. Sci.,2004
3. Sandhage, K. H. and Kumar, P. “Method for fabricating shaped monolithic ceramics and ceramic composites through displacive compensation of porosity, and ceramics and composites made thereby,” U. S. Patent No. 6,833,337, December 21, 2004.
4. Sandhage, K. H., Unocic, R. R., Dickerson, M. B., Timberlake, M., and Guerra, K., “Method for fabricating high-melting, wear-resistant ceramics and ceramic composites at low temperatures, U.S. Patent No. 6,598,656, July 29, 2003.
5. Ceramic-metal composites for heat exchangers in concentrated solar power plants;Caccia;Nature,2018