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二维振荡机翼跨声速非定常绕流的变域变分有限元解 被引量:4
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作者 郭加宏 刘高联 《空气动力学学报》 CSCD 北大核心 1996年第2期217-222,共6页
本文首先对文献[1~3]提出的二维振荡机翼含激波跨声速非定常绕流的变分原理进行了改造,使之能适用于时间推进法;构造了三维时空的可变节点有限元来捕获自由尾涡面,而跨声流中的激波采用人工密度法捕获。在远场边界上使用简化的... 本文首先对文献[1~3]提出的二维振荡机翼含激波跨声速非定常绕流的变分原理进行了改造,使之能适用于时间推进法;构造了三维时空的可变节点有限元来捕获自由尾涡面,而跨声流中的激波采用人工密度法捕获。在远场边界上使用简化的无反射条件和新型非定常Kutta条件。用本文方法求解了作俯仰振荡的NACA64A010翼型的跨声速绕流,计算结果令人满意。本文方法可以推广到三维机翼[4]及二维和三维叶栅的同类气动力问题上去。 展开更多
关键词 二维振荡 机翼流动 跨声速 非定常流 有限元
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Effect of fin attachment on thermal stress reduction of exhaust manifold of an off road diesel engine 被引量:4
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作者 Ali Akbar Partoaa Morteza Abdolzadeh Masoud Rezaeizadeh 《Journal of Central South University》 SCIE EI CAS CSCD 2017年第3期546-559,共14页
The effect of fin attachment on the thermal stress reduction of exhaust manifold of an off road diesel engine(Komatsu HD325-6) was investigated.For doing this,coupled thermo-fluid-solid analysis of exhaust manifold of... The effect of fin attachment on the thermal stress reduction of exhaust manifold of an off road diesel engine(Komatsu HD325-6) was investigated.For doing this,coupled thermo-fluid-solid analysis of exhaust manifold of the off road diesel engine was carried out.The thermal analysis,including thermal flow,thermal stress,and the thermal deformation of the manifold was investigated.The flow inside the manifold was simulated and then its properties including velocity,pressure,and temperature were obtained.The flow properties were transferred to the solid model and then the thermal stresses and the thermal deformations of the manifold under different operating conditions were calculated.Finally,based on the predicted thermal stresses and thermal deformations of the manifold body shell,two fin types as well as body shell thickness increase were applied in the critical induced thermal stress area of the manifold to reduce the thermal stress and thermal deformation.The results of the above modifications show that the combined modifications,i.e.the thickness increase and the fin attachment,decrease the thermal stresses by up to 28% and the contribution of the fin attachment in this reduction is much higher compared to the shell thickness increase. 展开更多
关键词 MANIFOLD EXHAUST simulation MODIFICATION thermal stress deformation diesel engine
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