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ASTM Selected Technical Papers
Composite Materials: Testing and Design (Ninth Volume)
By
SP Garbo
SP Garbo
1Sikorsky Aircraft Division,
United Technologies Corp.
, Stratford, CT 06601
; symposium chairman and editor
.
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ISBN-10:
0-8031-1287-4
ISBN:
978-0-8031-1287-2
No. of Pages:
598
Publisher:
ASTM International
Publication date:
1990
eBook Chapter
Composite Shear Moduli and Strengths from Torsion of Thick Laminates
Page Count:
13
-
Published:1990
Citation
Kurtz, R, & Sun, C. "Composite Shear Moduli and Strengths from Torsion of Thick Laminates." Composite Materials: Testing and Design (Ninth Volume). Ed. Garbo, S. 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959 : ASTM International, 1990.
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Composite bars of rectangular cross sections are loaded in torsion to determine the principal shear moduli and interlaminar strengths. The use of rectangular cross sections greatly simplifies the fabrication of specimens. In [0], [90], and cross-plied laminates, torsional rigidity depends only on the principal shear moduli and the dimensions of the cross section. Thus, the shear moduli can be determined from the measured torsional rigidity. This procedure proves very accurate and convenient in determining the transverse shear modulus G23. The use of this technique to measure in-plane shear and interlaminar strengths is also discussed in this paper.
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