Effect of cyclic loading and temper condition on the tensile behavior of boron-aluminum
Carl T. Herakovich, John M. Kennedy, Darrel R. Tenney
Abstract
Carl T. Herakovich, John M. Kennedy, Darrel R. Tenney
Abstract
Experimental results from monotonic and cyclic tension tests on six different 6061 boron-aluminum laminates show that the strength of fiber dominated laminates is decreased and the strength of matrix dominated laminates is increased by T6 heat treatment. Cyrogenic exposure and cyclic loading are shown to have little influence on strength. Cyclic loading is also shown to produce small reductions in modulus for some laminates and some temper conditions. The results are discussed in light of expected metallurgical and residual stress changes due to temperature excursions and loading cycles.
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Experimental results from monotonic and cyclic tension tests on six different 6061 boron-aluminum laminates show that the strength of fiber dominated laminates is decreased and the strength of matrix dominated laminates is increased by T6 heat treatment. Cyrogenic exposure and cyclic loading are shown to have little influence on strength. Cyclic loading is also shown to produce small reductions in modulus for some laminates and some temper conditions. The results are discussed in light of expected metallurgical and residual stress changes due to temperature excursions and loading cycles.
Key concepts: Materials science, Composite material, Ultimate tensile strength, Aluminium, Tension (geology), Boron, Modulus, Residual stress