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	Superplastic behavior of a Ni-Co-base superalloy with high gamma '-phase content 期刊论文 OAI收割 MATERIALS LETTERS, 2023, 卷号: 348, 页码: 4 作者: Al-Hammadi, Rashad A.; Zhang, Rui; Cui, Chuanyong; Zhou, Zijian; Zhou, Yizhou \| 收藏 \| 浏览/下载：10/0 \| 提交时间：2024/01/08 Superplasticity Metal and alloys Difficult-to-deform superalloy Microstructure gamma '-phase
	某铝合金复杂锻件成形工艺设计及DEFORM-3D模拟优化期刊论文 OAI收割锻压技术, 2018, 期号: 05, 页码: 154-161 作者: 王松伟; 张士宏; 陈岩; 宋鸿武 \| 收藏 \| 浏览/下载：34/0 \| 提交时间：2018/06/05 铝合金轻量化模具 Deform-3d数值模拟锻造工艺锻坯形状
	AZ31镁合金挤压无缝圆管混合晶粒有限元分析期刊论文 OAI收割轻金属, 2017, 期号: 1, 页码: 55-58 林涛; 刘运腾; 周吉学; 马百常; 杨院生收藏 \| 浏览/下载：35/0 \| 提交时间：2017/08/17 镁合金无缝圆管混合晶粒有限元 Deform
	基于Deform的镁合金薄壁方管挤压模具设计与改进期刊论文 OAI收割轻合金加工技术, 2016, 期号: 10, 页码: 41-45 林涛; 刘运腾; 唐守秋; 周吉学; 衣冠玉; 杨院生收藏 \| 浏览/下载：20/0 \| 提交时间：2016/12/28 镁合金薄壁方管模具 Deform稳态模拟挤压模具
	均匀化处理状态对Thermo-Span合金力学性能的影响会议论文 OAI收割于连旭; 孙文儒; 张周博; 张伟红; 刘芳; 信昕; 祁峰; 贾丹; 胡壮麒收藏 \| 浏览/下载：49/0 \| 提交时间：2016/04/20 Thermo-Span 均匀化处理先进航空发动机力学性能抗氧化性拉伸性能性能差异真空感应炉熔炼锻造开坯 deform
	A strong coupled CFD-CSD method on computational aeroelastity (EI CONFERENCE) 会议论文 OAI收割 2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011, July 15, 2011 - July 17, 2011, Inner Mongolia, China Xi R.; Jia H. 收藏 \| 浏览/下载：67/0 \| 提交时间：2013/03/25 In this paper a strong coupled CFD-CSD method is developed to simulate the aeroelastic phenomena. The CFD solver is based on the finite-volume algorithm for the Navier-Stokes equations on unstructured grid. The CSD solver solves the aeroelastic governing equations in the modal space. Their coupling is realized by a dual-time method. The spring-based smoothing method is adopted to deform and regenerate the aerodynamic grid. Two test cases are selected to validate the authors' method for static and dynamic aeroelastity .The results of the simulation for the static aeroelastic problems of a missile wing show that the Lift Coefficient and Drag Coefficient are severally 7% and 5% lower than those don't consider the elasticity of the wing. The results for the flutter boundary prediction of the AGARD 445.6 wing have been proved much closer to the experiment than using the DLM. This method can describe the effects of fluid viscosity more exactly for highly nonlinear transonic flight conditions. The calculation has proved reliable in the subsonic regime but not accurate enough in the supersonic regime. 2011 IEEE.
	25Cr2Ni4MoV钢的控温锻造会议论文 OAI收割 2006北京国际材料周暨中国材料研讨会, 北京, 2006-09 曹志远; 姜萍; 白云龙; 康秀红收藏 \| 浏览/下载：19/0 \| 提交时间：2013/08/21 25Cr2Ni4MoV钢控温锻造锻造变形 DEFORM软件动态再结晶形变热处理
	半轴套管锻造折迭问题的有限元模拟研究期刊论文 OAI收割热加工工艺, 2004, 期号: 2, 页码: 36-37+40 张伟红,张士宏,王忠堂,许沂,曲周德,安风军收藏 \| 浏览/下载：17/0 \| 提交时间：2012/04/12 DEFORM3D 半轴套管折迭有限元模拟