2018
DOI: 10.1016/j.procir.2018.05.033
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Experimental and FEM analysis of surface integrity when broaching Ti64

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Cited by 23 publications
(20 citation statements)
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“…49 For this reason, the development of machining simulations requires a material flow stress model, that governs the response of the deforming material. The workpiece material model is critical data for machining simulations with FEM 36,48 because it changes the system response in terms of cutting forces, temperature distribution and chip morphology. 50 The phenomenological models commonly used to simulate Ti6Al4V machining are presented in Table 1.…”
Section: Phenomenological Constitutive Models For Ti6al4v Machining Modelingmentioning
confidence: 99%
See 2 more Smart Citations
“…49 For this reason, the development of machining simulations requires a material flow stress model, that governs the response of the deforming material. The workpiece material model is critical data for machining simulations with FEM 36,48 because it changes the system response in terms of cutting forces, temperature distribution and chip morphology. 50 The phenomenological models commonly used to simulate Ti6Al4V machining are presented in Table 1.…”
Section: Phenomenological Constitutive Models For Ti6al4v Machining Modelingmentioning
confidence: 99%
“…[57][58][59][60][61][62] Those tests are performed under high strain, strain rate and temperature to replicate what happens to the material under machining conditions. 36,53,63 Table 1. Phenomenological constitutive models (highlighted in boldface) for machining modeling of Ti6Al4V.…”
Section: Phenomenological Constitutive Models For Ti6al4v Machining Modelingmentioning
confidence: 99%
See 1 more Smart Citation
“…The no-load condition is defined as the condition when the Strut Fin PMM attaches to the Towing Tank carriage without the load of the ship model below it. To assist the calculation of harmonic response using FEM software [10][11][12][13].…”
Section: Harmonic Response Analysismentioning
confidence: 99%
“…In 2016, Lu et al 28 employed a JC model coupled with Crock and Latham's (CL) failure criterion in DEFORM-2D TM to study the burr formation mechanism in Ti6Al4V OC operation. Similar modelling strategy was applied by Ortiz-de-Zarate et al 29 in 2018, the authors conducted numericalexperimental work to study the thickness of the deformed layer and the maximum residual compression stress in machined surfaces. They used models were created in DEFORM-2D TM using a JC law coupled with CL failure criterion.…”
Section: Introductionmentioning
confidence: 99%