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Simple torsion test for shear moduli determination of orthotropic compositesBy means of torsion tests performed on test specimens of the same material having a minimum of two different cross sections (flat sheet of different widths), the effective in-plane (G13) and out-of-plane (G23) shear moduli were determined for two composite materials of uniaxial and angleply fiber orientations. Test specimens were 16 plies (nominal 2 mm) thick, 100 mm in length, and in widths of 6.3, 9.5, 12.5, and 15.8 mm. Torsion tests were run under controlled deflection (constant angle of twist) using an electrohydraulic servocontrolled test system. In-plane and out-of-plane shear moduli were calculated from an equation derived in the theory of elasticity which relates applied torque, the torsional angle of twist, the specimen width/thickness ratio, and the ratio of the two shear moduli G13/G23. Results demonstrate that torsional shear moduli, G23 as well as G13, can be determined by simple torsion tests of flat specimens of rectangular cross section. Neither the uniaxial nor angleply composite material were transversely isotropic.
Document ID
19780013547
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sumsion, H. T.
(NASA Ames Research Center Moffett Field, CA, United States)
Rajapakse, Y. D. S.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1978
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-78485
A-7418
Report Number: NASA-TM-78485
Report Number: A-7418
Meeting Information
Meeting: Intern. Conf. on Composite Mater.
Location: Toronto
Start Date: April 16, 1978
End Date: April 20, 1978
Accession Number
78N21490
Funding Number(s)
PROJECT: RTOP 505-01-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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