Multiobjective optimization of process parameters of AZ91D/AgNPs/TiO2 composite fabricated by friction stir processing using response surface methodology and desirability

IF 1.2 4区 工程技术 Q3 ENGINEERING, AEROSPACE Aircraft Engineering and Aerospace Technology Pub Date : 2024-02-28 DOI:10.1108/aeat-07-2023-0196
Ram Niwas, Vikas Kumar
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Abstract

Purpose

This paper aims to determine the optimum parametric settings for yielding superior mechanical properties, namely, ultimate tensile strength (UTS), yield strength (YS) and percentage elongation (EL) of AZ91D/AgNPs/TiO2 hybrid composite fabricated by friction stir processing.

Design/methodology/approach

An empirical model has been developed to govern crucial influencing parameters, namely, rotation speed (RS), tool transverse speed (TS), number of passes (NPS) and reinforcement fraction (RF) or weight percentage. Box Behnken design (BBD) with four input parameters and three levels of each parameter was used to design the experimental work, and analysis of variance (ANOVA) was used to check the acceptability of the developed model. Desirability function analysis (DFA) for a multiresponse optimization approach is integrated with response surface methodology (RSM). The individual desirability index (IDI) was calculated for each response, and a composite desirability index (CDI) was obtained. The optimal parametric settings were determined based on maximum CDI values. A confirmation test is also performed to compare the actual and predicted values of responses.

Findings

The relationship between input parameters and output responses (UTS, YS, and EL) was investigated using the Box-Behnken design (BBD). Silver nanoparticles (AgNPs) and nano-sized titanium dioxide (TiO2) enhanced the ultimate tensile strength and yield strength. It was observed that the inclusion of AgNPs led to an increase in ductility, while the increase in the weight fraction of TiO2 resulted in a decrease in ductility.

Practical implications

AZ91D/AgNPs/TiO2 hybrid composite finds enormous applications in biomedical implants, aerospace, sports and aerospace industries, especially where lightweight materials with high strength are critical.

Originality/value

In terms of optimum value through desirability, the experimental trials yield the following results: maximum value of UTS (318.369 MPa), maximum value of YS (200.120 MPa) and EL (7.610) at 1,021 rpm of RS, 70 mm/min of TS, 4 NPS and level 3 of RF.

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利用响应面方法和可取性,多目标优化搅拌摩擦加工 AZ91D/AgNPs/TiO2 复合材料的工艺参数
目的 本文旨在确定最佳参数设置,以获得优异的机械性能,即通过搅拌摩擦加工制造的 AZ91D/AgNPs/TiO2 混合复合材料的极限拉伸强度 (UTS)、屈服强度 (YS) 和百分比伸长率 (EL)。实验设计采用箱式贝肯设计(BBD),有四个输入参数和每个参数的三个水平,并采用方差分析(ANOVA)来检查所开发模型的可接受性。多响应优化方法的可取性函数分析(DFA)与响应面方法(RSM)相结合。计算了每个响应的个别可取性指数(IDI),并得出了综合可取性指数(CDI)。根据 CDI 最大值确定最佳参数设置。此外,还进行了确认测试,以比较反应的实际值和预测值。研究结果采用方框-贝肯设计(BBD)研究了输入参数与输出反应(UTS、YS 和 EL)之间的关系。银纳米粒子(AgNPs)和纳米二氧化钛(TiO2)增强了极限拉伸强度和屈服强度。实际意义AZ91D/AgNPs/TiO2 混合复合材料在生物医学植入物、航空航天、体育和航天工业中有着广泛的应用,尤其是在对轻质高强度材料有严格要求的领域。原创性/价值在通过可取性实现最佳值方面,实验试验得出了以下结果:在 RS 1,021 rpm、TS 70 mm/min、4 NPS 和 RF 3 级条件下,UTS 的最大值(318.369 MPa)、YS 的最大值(200.120 MPa)和 EL 的最大值(7.610)。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Aircraft Engineering and Aerospace Technology
Aircraft Engineering and Aerospace Technology 工程技术-工程:宇航
CiteScore
3.20
自引率
13.30%
发文量
168
审稿时长
8 months
期刊介绍: Aircraft Engineering and Aerospace Technology provides a broad coverage of the materials and techniques employed in the aircraft and aerospace industry. Its international perspectives allow readers to keep up to date with current thinking and developments in critical areas such as coping with increasingly overcrowded airways, the development of new materials, recent breakthroughs in navigation technology - and more.
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