南京航空航天大学学报(英文版)
南京航空航天大學學報(英文版)
남경항공항천대학학보(영문판)
TRANSACTIONS OF NANJING UNIVERSITY OF AERONATICS & ASTRONAUTICS
2010年
3期
248-254
,共7页
汪洪峰%左敦稳%黄铭敏%陈明和%缪宏
汪洪峰%左敦穩%黃銘敏%陳明和%繆宏
왕홍봉%좌돈은%황명민%진명화%무굉
本构方程%塑性流动%弹塑性%温拉伸%7022铝合金
本構方程%塑性流動%彈塑性%溫拉伸%7022鋁閤金
본구방정%소성류동%탄소성%온랍신%7022려합금
constitutive equations%plastic flow%elastic-plastic%warm tension%7022 aluminum alloy
通过在293-773 K的温度范围内和应变速率为0.001-0.1 s-1下对7022铝合金薄板进行温拉伸试验,研究了7022铝合金温拉伸性能,以及该合金在升温条件下流变应力与变形温度和应变速率之间的关系.并利用改进了的Hooke law和Grosman方程建立了7022铝合金在温拉伸时应力-应变本构模型.研究结果表明:7022铝合金的流变应力随温度的升高而降低,随应变速率的升高而升高;温拉伸试样的延伸率随变形温度的升高而升高,随应变速率的增大而减小.
通過在293-773 K的溫度範圍內和應變速率為0.001-0.1 s-1下對7022鋁閤金薄闆進行溫拉伸試驗,研究瞭7022鋁閤金溫拉伸性能,以及該閤金在升溫條件下流變應力與變形溫度和應變速率之間的關繫.併利用改進瞭的Hooke law和Grosman方程建立瞭7022鋁閤金在溫拉伸時應力-應變本構模型.研究結果錶明:7022鋁閤金的流變應力隨溫度的升高而降低,隨應變速率的升高而升高;溫拉伸試樣的延伸率隨變形溫度的升高而升高,隨應變速率的增大而減小.
통과재293-773 K적온도범위내화응변속솔위0.001-0.1 s-1하대7022려합금박판진행온랍신시험,연구료7022려합금온랍신성능,이급해합금재승온조건하류변응력여변형온도화응변속솔지간적관계.병이용개진료적Hooke law화Grosman방정건립료7022려합금재온랍신시응력-응변본구모형.연구결과표명:7022려합금적류변응력수온도적승고이강저,수응변속솔적승고이승고;온랍신시양적연신솔수변형온도적승고이승고,수응변속솔적증대이감소.
Warm tensile tests for aluminum alloy 7022 sheet are held at different temperatures and strain rates.The range of temperature is 293-773 K and that of the strain rate is 0.001-0.1 s-1.The warm tensile properties,relations among temperature,strain rate,and the flow stress are discussed.Constitutive equations under the warm tension are obtained based on revised Hooke law and Grosman equation.It is concluded that flow stress declines with the increase of the temperature and the decrease of the strain rates.The elongation percentage increases with the increase of the temperature and the decrease of strain rate.