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内燃机机油泵工作特性数学模型的分析与研究 被引量:17
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作者 阮桢 胡德金 +3 位作者 许黎明 付则明 王海峰 冉丽红 《内燃机工程》 EI CAS CSCD 北大核心 2006年第3期50-53,57,共5页
通过对内燃机机油泵工作特性的分析,利用偏最小二乘回归法(PLSR)分析将内燃机机油泵工作特性数学模型由非线性关系式转化为内线性关系式,这既避免了数学模型信息的流失,又简化了数学模型回归系数的计算。通用特性试验的数据分析证明得... 通过对内燃机机油泵工作特性的分析,利用偏最小二乘回归法(PLSR)分析将内燃机机油泵工作特性数学模型由非线性关系式转化为内线性关系式,这既避免了数学模型信息的流失,又简化了数学模型回归系数的计算。通用特性试验的数据分析证明得到的内线性关系式是更优化的工作特性数学模型。 展开更多
关键词 内燃机 机油泵 工作特性 通用特性试验 偏最小二乘回归 主成分解释
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Tests and numerical simulation of aerodynamic characteristics of airfoils for general aviation applications
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作者 Zhang Lizhen Wang Xiaoming +1 位作者 Miguel A. Gonzáilez Hemáindez Wang Jun 《Engineering Sciences》 EI 2008年第4期71-74,共4页
This paper was to validate the effects of airfoil thickness ratio on the characteristics of a family of airfoils. Research was carried out in different ways. First,tests were conducted in the wind tunnel. And numerica... This paper was to validate the effects of airfoil thickness ratio on the characteristics of a family of airfoils. Research was carried out in different ways. First,tests were conducted in the wind tunnel. And numerical simulation was performed on the basis of tests. Results from calculation were consistent with tests,indicating that numerical method could help evaluate characteristics of airfoils. Then the results were confirmed by compared with empirical data. The study also showed that the determining factor of lift is not only the thickness ratio,but the angle of attack,the relative camber and the camber line. The thickness ratio appears to have little effect on lift coefficient at zero angle of attack,since the angle of zero lift is largely determined by the airfoil camber. According to the research,numerical simulation can be used to determine the aerodynamic characteristics of airfoils in different environment such as in the dusty or humid air. 展开更多
关键词 aerodynamic characteristics numerical simulation AIRFOIL thickness ratio
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