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Processing eutectics in spaceExperimental work is reported which was directed toward obtaining interface shape control while a numerical thermal analysis program was being made operational. An experimental system was developed in which the solid-liquid interface in a directionally solidified aluminum-nickel eutectic could be made either concave to the melt or convex to the melt. This experimental system provides control over the solid-liquid interface shape and can be used to study the effect of such control on the microstructure. The SINDA thermal analysis program, obtained from Marshall Space Flight Center, was used to evaluate experimental directional solidification systems for the aluminum-nickel and the aluminum-copper eutectics. This program was applied to a three-dimensional ingot, and was used to calculate the thermal profiles in axisymmetric heat flow. The results show that solid-liquid interface shape control can be attained with physically realizable thermal configurations and the magnitudes of the required thermal inputs were indicated.
Document ID
19750006719
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Douglas, F. C.
(United Aircraft Corp. East Hartford, CT, United States)
Galasso, F. S.
(United Aircraft Corp. East Hartford, CT, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1974
Subject Category
Astronautics (General)
Report/Patent Number
NASA-CR-120569
N911721-S/A2-4
Report Number: NASA-CR-120569
Report Number: N911721-S/A2-4
Accession Number
75N14791
Funding Number(s)
CONTRACT_GRANT: NAS8-29669
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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