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Matrix density effects on the mechanical properties of SiC/RBSN compositesThe room temperature mechanical properties were measured for SiC fiber reinforced reaction-bonded silicon nitride composites (SiC/RBSN) of different densities. The composites consisted of approx. 30 vol percent uniaxially aligned 142 micron diameter SiC fibers (Textron SCS-6) in a reaction-bonded Si3N4 matrix. The composite density was varied by changing the consolidation pressure during RBSN processing and by hot isostatically pressing the SiC/RBSN composites. Results indicate that as the consolidation pressure was increased from 27 to 138 MPa, the average pore size of the nitrided composites decreased from 0.04 to 0.02 microns and the composite density increased from 2.07 to 2.45 gm/cc. Nonetheless, these improvements resulted in only small increases in the first matrix cracking stress, primary elastic modulus, and ultimate tensile strength values of the composites. In contrast, HIP consolidation of SiC/RBSN resulted in a fully dense material whose first matrix cracking stress and elastic modulus were approx. 15 and 50 percent higher, respectively, and ultimate tensile strength values were approx. 40 percent lower than those for unHIPed SiC/RBSN composites. The modulus behavior for all specimens can be explained by simple rule-of-mixture theory. Also, the loss in ultimate strength for the HIPed composites appears to be related to a degradation in fiber strength at the HIP temperature. However, the density effect on matrix fracture strength was much less than would be expected based on typical monolithic Si3N4 behavior, suggesting that composite theory is indeed operating. Possible practical implications of these observations are discussed.
Document ID
19900012510
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bhatt, Ramakrishna T.
(Army Aviation Systems Command Cleveland, OH., United States)
Kiser, James D.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1990
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-103098
AD-A224494
E-5306
AVSCOM-TR-90-C-008
NAS 1.15:103098
Report Number: NASA-TM-103098
Report Number: AD-A224494
Report Number: E-5306
Report Number: AVSCOM-TR-90-C-008
Report Number: NAS 1.15:103098
Meeting Information
Meeting: Annual Conference on Composites and Advanced Ceramics
Location: Cocoa Beach, FL
Country: United States
Start Date: January 14, 1990
End Date: January 17, 1990
Sponsors: American Ceramic Society
Accession Number
90N21826
Funding Number(s)
PROJECT: RTOP 510-01-0A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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