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Residual stress and mechanical properties analysis of TC4 alloy fabricated by laser additive manufacturing
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作者 ZHAO Hong-jian LIU Chen +4 位作者 HU Jie-xin YIN Shuai YANG Chao-wei LIU Chang-sheng ZHAN Yu 《Journal of Central South University》 CSCD 2024年第11期3983-3995,共13页
Large residual stresses would be generated in the laser additive manufactured(LAMed)structures after processing rapid and intense heating and cooling cycles with bad mechanical properties.Scholars have tried many meth... Large residual stresses would be generated in the laser additive manufactured(LAMed)structures after processing rapid and intense heating and cooling cycles with bad mechanical properties.Scholars have tried many methods to decrease the residual stress to prevent the structures from being broken and improve the mechanical properties.In this study,residual stress and mechanical properties of LAMed structures are analyzed,and the advanced measuring method,laser ultrasonic technique,is used to detect the residual stresses accumulated in the samples in time.The results show that when the solution temperature is less than T_(β)(992℃),the residual stress increases gradually with the increase of solution temperature,and when the temperature is more than T_(β)(992℃),Widmanstätten structure will significantly reduce the residual stress;the mechanical properties of the specimen decrease with the increase of the solution temperature,and the different cooling methods do not have much effect on the elastic properties of the specimen.Considering the residual stress and mechanical properties,the HT1 system used in this paper is the best.This study is of great significance for the reasonable suppression of residual stress and the regulation of mechanical properties of TC4 titanium alloy fabricated by laser additive manufacturing. 展开更多
关键词 laser additive manufacturing heat treatment residual stress mechanical properties
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Six-DOF trajectory optimization for reusable launch vehicles via Gauss pseudospectral method 被引量:5
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作者 Zhen Wang Zhong Wu 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 2016年第2期434-441,共8页
To be close to the practical flight process and increase the precision of optimal trajectory, a six-degree-offreedom(6-DOF) trajectory is optimized for the reusable launch vehicle(RLV) using the Gauss pseudospectr... To be close to the practical flight process and increase the precision of optimal trajectory, a six-degree-offreedom(6-DOF) trajectory is optimized for the reusable launch vehicle(RLV) using the Gauss pseudospectral method(GPM). Different from the traditional trajectory optimization problem which generally considers the RLV as a point mass, the coupling between translational dynamics and rotational dynamics is taken into account. An optimization problem is formulated to minimize a performance index subject to 6-DOF equations of motion, including translational and rotational dynamics. A two-step optimal strategy is then introduced to reduce the large calculations caused by multiple variables and convergence confinement in 6-DOF trajectory optimization. The simulation results demonstrate that the 6-DOF trajectory optimal strategy for RLV is feasible. 展开更多
关键词 reusable launch vehicle(RLV) trajectory optimization Gauss pseudospectral method(GPM)
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