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叶型中弧线的最大弯度位置对跨音速压气机叶片性能影响的研究 被引量:4
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作者 陈乃兴 张宏武 +1 位作者 徐燕骥 黄伟光 《工程热物理学报》 EI CAS CSCD 北大核心 2005年第3期409-412,共4页
本文研究与分析了叶型中弧线的最大弯度位置对跨音速压气机叶片气动性能的影响。采取了注重流动机理的优化方法,对本文算例的风扇叶片进行了优化,改进后所得的叶片的效率比原设计有了较大的提高。
关键词 跨音速压气机气动设计 叶型中弧线最大弯度位置 叶片优化设计
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跨音速单转子压气机气动设计的优化 被引量:2
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作者 张宏武 陈乃兴 +1 位作者 徐燕骥 黄伟光 《工程热物理学报》 EI CAS CSCD 北大核心 2005年第4期581-583,共3页
本文发展了一种提高跨音压气机效率的优化设计方法。该方法由快速叶片造型和网格生成、三维NS方程求解器和优化方法三部分组成。以绝热效率为设计目标,只选择两个参数-最大弯度和最大厚度相对位置沿叶高的分布为优化参数,成功设计了一... 本文发展了一种提高跨音压气机效率的优化设计方法。该方法由快速叶片造型和网格生成、三维NS方程求解器和优化方法三部分组成。以绝热效率为设计目标,只选择两个参数-最大弯度和最大厚度相对位置沿叶高的分布为优化参数,成功设计了一个跨音单转子压气机。在此基础上,进一步考察了叶片端布周向弯曲对跨音单转子压气机性能的影响。 展开更多
关键词 最大弯度 最大厚度 优化设计
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Calculation method of first collapse span with superhigh water material backfill mining 被引量:3
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作者 ZHANG Li-ya DENG Ka-zhong 《Journal of Coal Science & Engineering(China)》 2012年第4期374-378,共5页
It is critical for the material to be of active supporting capacity before initial collapse ot mare root wltn supermgn water material backfill mining, and the maximum bending moment should be first calculated in order... It is critical for the material to be of active supporting capacity before initial collapse ot mare root wltn supermgn water material backfill mining, and the maximum bending moment should be first calculated in order to determine the initial collapse span. In the light of principal of virtual work, the simple expression of deflection, bending moment of elastic clamped plate were deduced under the condition of vertical uniform distributed load, horizontal pressure and supporting by elastic foundation, and then, the maximal bending moment expression was derived too. At the same time, the influence degree on square clamped plate by adding horizontal pressure and elastic foundation were analyzed. The results show that the effect of horizontal pressure on maximal bending moment can be ignored when the value of horizontal pressure is two orders of magni- tude less than that of coeificient of elastic stiffness existing elastic foundation. 展开更多
关键词 first collapse span superhigh water material backfill mining elastic clamped plate principal of virtual work
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The influence of Fe extracting as a filler of fiber concrete performance
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作者 Nawir Rasidi 《Journal of Civil Engineering and Architecture》 2009年第5期46-52,共7页
This research is showing the effect of increasing an Fe extracting from the compression strength, tension and bending moment. The variations in this experiment are the increasing of Fe extracting 0.5%, 1% and 1.5% of ... This research is showing the effect of increasing an Fe extracting from the compression strength, tension and bending moment. The variations in this experiment are the increasing of Fe extracting 0.5%, 1% and 1.5% of concrete volume. Water Cement Ratio (WCR) variation of 0.48, 0.56 and 0.60. The result of increasing 1.5% Fe extracting causes the increasing of tension strength 44.028 kN/cm2, the increasing of slit tension strength 2.226 kN/cm2, the increasing of bending moment 14.81 kN/cm2 from normal concrete. 0.48 WCR produces tension strength, slit tension strength and bending moment more than 0.56 and 0.60 WCR. The increasing of Fe extracting with the distribution variation area and the spread concrete in the tension concrete area produce 3.705 kN/cm2 bending moment higher than the spread fiber in all of concrete area. The 4 cm fiber length produces the higher bending moment than the 2 cm fiber length. The difference is equally 5.185 kN/cm2. The combination result of the examined acting varieties by continuation statistic test gives the result to get the maximum tension and split tensile. It is a concrete combination of increasing 1.5% fiber percentage, 0.48 WCR, full spreading area and the 4 cm fiber length. The maximum bending moment is the increasing of 0.5% fiber percentage, 0.48 WCR, full spreading area and the 4 cm fiber length. 展开更多
关键词 Fe extracting fiber concrete performance acting combination
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Analysis and Improvement of Standing-Up Action for Elderly People from a Chair Using a Cushion-Type Support Tool
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作者 Masakazu Takahashi Reiji Nanba 《Computer Technology and Application》 2012年第11期713-722,共10页
This paper reports the problems that elderly people have when they stand up from a chair, and proposes an adequate standing-up procedure that solves these problems. The important points for an adequate standing-up pro... This paper reports the problems that elderly people have when they stand up from a chair, and proposes an adequate standing-up procedure that solves these problems. The important points for an adequate standing-up procedure are "leaning the upper body forward" and "pulling the legs to the side". Furthermore, this paper proposes a standing-up support tool. The characteristics of the support tool are a cushion-type shape with an adjustable flange and an air-pressure-driven mechanism. When the proposed standing-up procedure and support tool are applied to elderly people, the measured values related to standing-up, such as maximum acceleration, arm force, standing-up time, heel position and forward-bending angle, are improved. Furthermore, elderly people felt that it made the standing-up action easy. We could confirm the effectiveness of the proposed standing-up procedure and support tool. 展开更多
关键词 Elderly people standing-up procedure standing-up support tool cushion-type shape air-pressure-driven mechanism.
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桨叶翼型弯度对摆线桨悬停状态的气动性能影响
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作者 钱悦 黄典贵 《航空动力学报》 EI CAS CSCD 北大核心 2018年第6期1500-1509,共10页
以悬停状态下的摆线桨为研究对象,利用数值模拟方法,分别研究了桨叶相对弯度X和最大弯度位置Y对摆线桨气动性能的影响。结果表明:与桨叶为对称翼型的摆线桨相比,当桨叶具有一定弯度且最大弯度位置适中时,摆线桨气动性能得到很大的提升... 以悬停状态下的摆线桨为研究对象,利用数值模拟方法,分别研究了桨叶相对弯度X和最大弯度位置Y对摆线桨气动性能的影响。结果表明:与桨叶为对称翼型的摆线桨相比,当桨叶具有一定弯度且最大弯度位置适中时,摆线桨气动性能得到很大的提升。当桨叶相对弯度X为4%C(C为翼型弦长)、最大弯度位置Y距离前缘40%C^50%C时,摆线桨升力和气动功耗比较低,悬停效率最高,整体气动性能更好。 展开更多
关键词 摆线桨 悬停 相对弯度 最大弯度位置 气动性能
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桨叶翼型弯度对摆线桨前飞状态气动性能的影响
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作者 钱悦 黄典贵 《热能动力工程》 CAS CSCD 北大核心 2018年第6期26-33,65,共9页
以前飞状态下的摆线桨为研究对象,使用CFD软件进行数值模拟,非定常时间推进采用双时间法,计算模型的刚体运动采用滑移网格技术处理,分别研究了桨叶相对弯度X和最大弯度位置Y对摆线桨气动性能的影响。研究表明:与桨叶为对称翼型的摆线... 以前飞状态下的摆线桨为研究对象,使用CFD软件进行数值模拟,非定常时间推进采用双时间法,计算模型的刚体运动采用滑移网格技术处理,分别研究了桨叶相对弯度X和最大弯度位置Y对摆线桨气动性能的影响。研究表明:与桨叶为对称翼型的摆线桨相比,当桨叶具有一定的弯度且最大弯度位置适中时,推力和推进效率都有显著提高;随着相对弯度的增加,推进效率先增大后减小,存在一个最佳的相对弯度X使得推进效率最高;随着最大弯度位置向尾缘移动,相对弯度X=2%C时,推进效率缓慢上升,相对弯度X〉2%C时,推进效率先增大后减小,存在一个最佳的最大弯度位置Y使得推进效率最高,但升力和载重系数都有所下降。实际应用时,需综合考虑飞行器实际载重确定合适的桨叶弯度。 展开更多
关键词 摆线桨 前飞 相对弯度 最大弯度位置 气动性能
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绕线轮的选购与使用
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作者 谭佛航 《中国钓鱼》 1999年第3期23-23,共1页
关键词 绕线轮 曳力 收放线 钓线 绕线轴 操作方法 开关 收线 旋压 最大弯度
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A Study of 3D Aerodynamic Design for a Transonic Compressor Blading Optimized by the Locations of Aerofoil Maximum Thickness and Maximum Camber 被引量:1
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作者 Naixing Chen Hongwu Zhang Yanji Xu Weiguang HuangInstitute of Engineering Thermophysics, Chinese Academy of Sciences, P.O. Box 2706, Beijing 100080, 《Journal of Thermal Science》 SCIE EI CAS CSCD 2003年第3期198-203,共6页
A design procedure for improving the efficiency of a transonic compressor blading was proposed based on a rapid generation method for three-dimensional blade configuration and computational meshes, a three-dimensional... A design procedure for improving the efficiency of a transonic compressor blading was proposed based on a rapid generation method for three-dimensional blade configuration and computational meshes, a three-dimensional Navier-Stokes solver and an optimization approach. The objective of the present paper is to design a transonic compressor blading optimized only by selection of the locations of maximum camber and maximum thickness for the airfoils at different span heights and to study how do these two design parameters affect the blade performance. The blading configuration and the computational meshes can be obtained very rapidly for any given combination of maximum camber and maximum thickness. The computational grid system generated is used for the Navier-Stokes solution to predict adiabatic efficiency, total pressure ratio and flow rate. As a main result of the optimization, adiabatic efficiency was successfully improved. 展开更多
关键词 axial transonic compressor 3D aerodynamic design optimization N.S. solver rapid generation of computational meshes
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Aerodynamic/mechanism optimization of a variable camber Fowler flap for general aviation aircraft 被引量:1
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作者 TIAN Yun WANG Tao +1 位作者 LIU PeiQing FENG PeiHua 《Science China(Technological Sciences)》 SCIE EI CAS CSCD 2017年第8期1144-1159,共16页
A conventional Fowler flap is designed to improve the take-off and landing performances of an aircraft. Because the flight states of general aviation aircraft vary significantly. A Fowler flap with a double-sliding tr... A conventional Fowler flap is designed to improve the take-off and landing performances of an aircraft. Because the flight states of general aviation aircraft vary significantly. A Fowler flap with a double-sliding track has been designed, which is ca- pable of changing airfoil camber while cruising and climbing as well as meeting low-speed performance requirements. The aerodynamic characteristics of the variable camber Fowler flap were studied by computational simulation, and cambering was found to be beneficial for improving the lift-to-drag ratio when the lift coefficient was larger than the critical value, below which decambering was more effective; this critical value differed somewhat under different conditions. Taking the mecha- nism into account, the take-off and landing configurations were optimized on the basis of the GA (W)-1 airfoil with a 30% chord Fowler flap. Compared with reference configuration, the maximum lift coefficient of optimized take-off configuration was increased by 6.6% as well as the stalling angle and the lift-to-drag ratio were increased by 1.3° and 7.58%, respectively. Moreover, the maximum lift coefficient of the optimized landing configuration was increased by 6.3%, and the stalling angle was increased by 1.1°; however, the nose-down pitching moment of both configurations increased. Similar results were at- rained on a general aviation aircraft wing/body combination nism was established in a computer-aided design system, achieved by the double-sliding track. A 3D model of the variable-camber Fowler flap driving mecha- and the results showed that all design configurations could be 展开更多
关键词 Fowler flap general aviation aircraft variable camber OPTIMIZATION
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