航空计算技术
航空計算技術
항공계산기술
Aeronautical Computing Technique
2015年
5期
5-7,10
,共4页
蠕变应变%模型参数反演%优化方法%Norton-Bailey蠕变模型%Prandtl-Garofalo蠕变模型
蠕變應變%模型參數反縯%優化方法%Norton-Bailey蠕變模型%Prandtl-Garofalo蠕變模型
연변응변%모형삼수반연%우화방법%Norton-Bailey연변모형%Prandtl-Garofalo연변모형
creep strain%model parameter estimation%optimization algorithm%Norton-Bailey creep model%Prandtl-Garofalo creep model
基于铝合金材料单轴拉伸蠕变实验观测数据,提出了铝合金材料蠕变模型参数优化反演方法。针对3种典型的铝合金材料,分别反演确定了Norton-Bailey和Prandtl-Garofalo蠕变模型中的参数。计算结果表明,蠕变应变与时间的(0.2~0.4)次幂成正比,与等效应力的(6.0~7.6)次幂成正比。对于7050和7 B04铝合金材料, Prandtl-Garofalo蠕变模型给出了较高的预测精度。对于7075铝合金材料,Norton-Bailey蠕变模型给出了较高的预测精度。铝合金材料蠕变模型预测的应变与实验值基本一致,验证了所提出模型参数反演方法的有效性。
基于鋁閤金材料單軸拉伸蠕變實驗觀測數據,提齣瞭鋁閤金材料蠕變模型參數優化反縯方法。針對3種典型的鋁閤金材料,分彆反縯確定瞭Norton-Bailey和Prandtl-Garofalo蠕變模型中的參數。計算結果錶明,蠕變應變與時間的(0.2~0.4)次冪成正比,與等效應力的(6.0~7.6)次冪成正比。對于7050和7 B04鋁閤金材料, Prandtl-Garofalo蠕變模型給齣瞭較高的預測精度。對于7075鋁閤金材料,Norton-Bailey蠕變模型給齣瞭較高的預測精度。鋁閤金材料蠕變模型預測的應變與實驗值基本一緻,驗證瞭所提齣模型參數反縯方法的有效性。
기우려합금재료단축랍신연변실험관측수거,제출료려합금재료연변모형삼수우화반연방법。침대3충전형적려합금재료,분별반연학정료Norton-Bailey화Prandtl-Garofalo연변모형중적삼수。계산결과표명,연변응변여시간적(0.2~0.4)차멱성정비,여등효응력적(6.0~7.6)차멱성정비。대우7050화7 B04려합금재료, Prandtl-Garofalo연변모형급출료교고적예측정도。대우7075려합금재료,Norton-Bailey연변모형급출료교고적예측정도。려합금재료연변모형예측적응변여실험치기본일치,험증료소제출모형삼수반연방법적유효성。
In order to estimate parameters of creep models of aluminum alloy materials,a parameter inver-sion procedure is proposed with optimization algorithm,which is based on uniaxial tension creep experi-ments for aluminum alloy materials.For three kinds of aluminum alloy materials,the parameters of creep models both for Norton-Bailey and Prandtl-Garofalo creep model are determined.The investigation shows that the time exponent (γ+1) in creep model changes from 0.2 to 0.4,and the equivalent stress expo-nent (β) in creep model changes from 6.0 to 7.6.For 7050 and 7B04 aluminum alloy materials,Prandtl-Garofalo creep model shows higher forecasting precision.For 7075 aluminum alloy material,Norton-Bai-ley creep model shows higher forecasting precision.The forecasting creep strains based on estimated pa-rameters of creep models agree well with observed ones.The effectiveness of proposed parameter estima-ting procedure of creep models of aluminum alloy materials is validated from experimental data.