Conference paper
True 3-D displays for avionics and mission crewstations
Elizabeth A. Sholler, Frederick M. Meyer, et al.
SPIE AeroSense 1997
A model describing the salient features of tensile stress‐strain curves of ceramic–fiber composites has been developed. The model incorporates statistics of fiber failure. Furthermore, the compliance of the testing machine is included so that the onset of instability can be predicted. An experiment conducted on a composite consisting of a glass‐ceramic matrix reinforced with SiC fibers exhibits excellent agreement with the predicted behavior. Copyright © 1990, Wiley Blackwell. All rights reserved
Elizabeth A. Sholler, Frederick M. Meyer, et al.
SPIE AeroSense 1997
E. Burstein
Ferroelectrics
Daniel J. Coady, Amanda C. Engler, et al.
ACS Macro Letters
T. Schneider, E. Stoll
Physical Review B