NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
High Temperature Tensile Properties of Unidirectional Hi-Nicalon/Celsian Composites In AirHigh temperature tensile properties of unidirectional BN/SiC-coated Hi-Nicalon SiC fiber reinforced celsian matrix composites have been measured from room temperature to 1200 C (2190 F) in air. Young's modulus, the first matrix cracking stress, and the ultimate strength decreased from room temperature to 1200 C (2190 F). The applicability of various micromechanical models, in predicting room temperature values of various mechanical properties for this CMC, has also been investigated. The simple rule of mixtures produced an accurate estimate of the primary composite modulus. The first matrix cracking stress estimated from ACK theory was in good agreement with the experimental value. The modified fiber bundle failure theory of Evans gave a good estimate of the ultimate strength.
Document ID
20000085860
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Gyekenyesi, John Z.
(Ohio Aerospace Inst. Brook Park, OH United States)
Bansal, Narottam P.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
September 7, 2013
Publication Date
July 1, 2000
Subject Category
Composite Materials
Report/Patent Number
NASA/TM-2000-210214
NAS 1.15:210214
E-12333
Report Number: NASA/TM-2000-210214
Report Number: NAS 1.15:210214
Report Number: E-12333
Funding Number(s)
PROJECT: RTOP 523-75-13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available