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Evaluations of filament-reinforced composites for aerospace structural applicationsElastic constant, tensile, and compressive strength analysis for structural efficiency study of filament reinforced sandwich cylindrical shell
Document ID
19650012756
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Dow, N. F. (General Electric Co. Philadelphia, PA, United States)
Rosen, B. W. (General Electric Co. Philadelphia, PA, United States)
Date Acquired
August 2, 2013
Publication Date
April 1, 1965
Subject Category
Materials, Nonmetallic
Report/Patent Number
NASA-CR-207
Report Number: NASA-CR-207
Accession Number
65N22357
Funding Number(s)
CONTRACT_GRANT: NASW-817
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CYLINDRICAL SHELL
FILAMENT WINDING
ELASTIC CONSTANT
TENSILE STRENGTH
REINFORCED MATERIAL

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