Material Parameter Modification for Age Forming Simulation Based on Response Surface Model

熊威; 甘忠; 许旭东

doi:10.16080/j.issn1671-833x.2011.19.017

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Material Parameter Modification for Age Forming Simulation Based on Response Surface Model

更新时间：2026-04-23

- Material Parameter Modification for Age Forming Simulation Based on Response Surface Model
- Aeronautical Manufacturing Technology Vol. 54, Issue 19, Pages: 80-83(2011)
- 作者机构：
  
  1. 西北工业大学现代设计与集成制造技术教育部重点实验室
  2. 中航工业成都飞机工业（集团）有限责任公司制造工程部
- 作者简介：
- 基金信息：
- DOI：10.16080/j.issn1671-833x.2011.19.017
  CLC：
- Published：2011
- 稿件说明：
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熊威，甘忠，许旭东. 基于响应曲面的时效成形材料参数修正[J]. 航空制造技术, 2011, 54(19): 80-83.

熊威, 甘忠, 许旭东. Material Parameter Modification for Age Forming Simulation Based on Response Surface Model[J]. Aeronautical Manufacturing Technology, 2011, 54(19): 80-83.
熊威，甘忠，许旭东. 基于响应曲面的时效成形材料参数修正[J]. 航空制造技术, 2011, 54(19): 80-83. DOI： 10.16080/j.issn1671-833x.2011.19.017.

熊威, 甘忠, 许旭东. Material Parameter Modification for Age Forming Simulation Based on Response Surface Model[J]. Aeronautical Manufacturing Technology, 2011, 54(19): 80-83. DOI： 10.16080/j.issn1671-833x.2011.19.017.

摘要

为了提高时效成形中回弹现象的有限元仿真精度，使用均匀试验设计结合响应曲面设计的方法，建立了仿真误差对于材料参数的响应函数，求解出材料参数的修正解。以此法得到的仿真结果与试验结果相吻合。

Abstract

A modifi ed solution of material parameters is obtained by solving simulation error response function for material parameters

which is established by response surface methods combined with uniform design

in order to improve finite element analysis precise for springback in creep age forming. The simulation results with the modifi ed solution are in accord with experimental results.

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