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A more comprehensive method for yield locus construction for metallic alloys and composites

机译:一种用于金属合金和复合材料的屈服点构建的更全面的方法

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Conventional methods for constructing yield loci rely on the assumption that nonlinear strains are permanent strains, which is not always the case. A nickel-base alloy, SiC fiber-reinforced titanium, an aluminum alloy, and particlereinforced aluminum have been observed to violate this assumption. We present a method for constructing yield loci using a proof strain criterion for the permanent strain that relies on cyclic, proportional, probes of the yield surface. Two criteria are implemented: one for stress reversal and one for yielding. The method is demonstrated by the construction of initial and subsequent yield loci in the axial-shear stress plane using thin-walled tubular specimens. Results are presented for 6061-T6 aluminum as well as for 6092/SiC/17.5p-T6, which is 6092 aluminum reinforced with 17.5 volume percent silicon carbide particulate. The centers of the initial yield loci for the composite are eccentric to the origin of the stress plane most likely because of the residual stresses induced during processing. Material hardening due to multiaxial stress states can be described by tracking evolution of the subsequent yield surfaces and here hardening of the particulate composite was primarily kinematic
机译:构造屈服位点的常规方法依赖于以下假设:非线性应变是永久应变,并非总是如此。已经观察到镍基合金,SiC纤维增强钛,铝合金和颗粒增强铝违反了这一假设。我们提出了一种使用依赖于屈服面的周期性,成比例探针的永久应变的证明应变准则来构建屈服位点的方法。实施了两个标准:一个用于逆转应力,一个用于屈服。该方法通过使用薄壁管状试样在轴向剪切应力平面上构造初始和后续屈服位点来证明。给出了6061-T6铝以及6092 / SiC / 17.5p-T6的结果,后者是用17.5体积百分比的碳化硅颗粒增强的6092铝。复合材料的初始屈服点的中心最有可能相对于应力平面的原点是偏心的,这是因为在加工过程中会产生残余应力。可以通过跟踪后续屈服面的演变来描述由于多轴应力状态引起的材料硬化,此处颗粒复合材料的硬化主要是运动学上的

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