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A numerical analysis of restrained shrinkage stresses in ablation heat shieldsNumerical analysis of restrained shrinkage stresses in ablation heat shields
Document ID
19690030835
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Dow, M. B. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1969
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-X-61915
Report Number: NASA-TM-X-61915
Accession Number
69N40220
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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