journal article·1969-04

The Solid-Rod Torsion Test for the Determination of Unidirectional Composite Shear Properties

Donald F. Adams, Rodney L. Thomas

Textile Research Journal· Volume 39· Issue 4
Publisher page

Abstract

The primary requirements of a desirable shear test method include the ability to introduce a well-defined state of stress in the specimen, capability of determining both shear modulus and shear strength with one test of a single specimen, use of a minimum amount of material per specimen, ease of specimen fabrication and preparation, and simplicity of testing. The solid-rod torsion test is shown to fulfill these requirements. Methods and equipment developed for both the fabrication and testing of specimens are discussed in detail. Experimental data obtained by utilizing the solid-rod torsion test on several different, composite-material systems are presented. These results are then compared with data obtained by utilizing other shear-property test methods.
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Research context

OpenAlex topics: Metal Forming Simulation Techniques · Structural Load-Bearing Analysis · High-Velocity Impact and Material Behavior

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

The RAND Corporation, Santa Monica, California 90406, U. S. A.

Washington University, St. Louis, Missouri 63130, U. S. A.

References (6)

Show source-provided references
1. 10.1177/00219983670010010210.1177/002199836700100102 ↗
2. Adams D. F., Doner D. R., Thomas R. L. “Mechanical Behavior of Fiber-Reinforced Composite Materials,” Air Force Materials Laboratory Technical Report AFML-TR-67-96, May 1967.
3. Adams D. F., Thomas R. L. “Test Methods for the Determination of Unidirectional Composite Shear Properties,” Proceedings of the Twelfth National SAMPE Symposium—Advances in Structural Composites, October 1967.
4. Douglas Aircraft, Inc. “Crazing and Yielding of Reinforced Composites,” Air Force Materials Laboratory Contract No. AF 33(615)-3931, Third Quarterly Progress Report, March 1967.
5. Novak R. C. “Investigation of Graphite Filament Reinforced Epoxies,” Final Report, Naval Air Systems Command Contract N00019-67-C-0354, Philco-Ford Corporation, Aeronutronic Division Publication No. U-4379, May 1968, pp. 23–25.
6. Wilson F. M. “Research on Resin-Impregnated, Collimated Boron Filaments and Improved High-Modulus, High-Strength Filaments and Composites,” Air Force Materials Laboratory Technical Report AFML-TR-67-20, January, 1967.