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Transverse tensile and stress rupture properties of gamma/gamma prime-delta directionally solidified eutecticTensile and stress rupture properties were determined primarily at 760 C for specimens oriented at various angles (0 deg, 10 deg, 45 deg, and 90 deg) from the solidification direction of bars and/or slabs of the Ni-20Cb-6Cr-2.5A (gamma/gamma prime-delta) eutectic. Threaded-head specimens yielded longer rupture lives with significantly less scatter than did tapered-head specimens. Miniature specimens are suitable for determining traverse tensile and rupture properties of 1.2 centimeter diameter bar stock. The 300 hour rupture stress at 760 C for specimens oriented at 10 deg from the solidification direction was reduced from 740 to 460 MPa, and to 230 MPa for material oriented at either 45 deg or 90 deg.
Document ID
19760026226
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Gray, H. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1976
Subject Category
Metallic Materials
Report/Patent Number
E-8810
NASA-TM-X-73451
Report Number: E-8810
Report Number: NASA-TM-X-73451
Accession Number
76N33314
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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