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三角形空翼缘梁的极限承载力试验研究 被引量:3
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作者 魏建军 宋生志 《土木建筑与环境工程》 CSCD 北大核心 2014年第3期106-111,共6页
在澳大利亚学者提出的空翼缘梁(HFB)的基础上,提出一种新型三角形空翼缘梁(THFB)。通过试验测试,对三角形空翼缘梁(THFB)和传统H型钢梁在承受集中荷载作用下的破坏过程进行了对比,发现两种梁的破坏模态存在明显差异,THFB在集中荷载作用... 在澳大利亚学者提出的空翼缘梁(HFB)的基础上,提出一种新型三角形空翼缘梁(THFB)。通过试验测试,对三角形空翼缘梁(THFB)和传统H型钢梁在承受集中荷载作用下的破坏过程进行了对比,发现两种梁的破坏模态存在明显差异,THFB在集中荷载作用下极易发生局部屈曲,传统H型钢梁则易发生整体失稳,且THFB比传统H型钢梁具有较好的抗弯扭性能。利用有限元软件ANSYS对试验试件进行有限元模拟,试验结果和有限元模拟结果吻合较好。基于所建的有限元模型对THFB进行参数分析,参数主要包括上翼缘板厚、上翼缘板宽、腹板厚和钢材屈服强度,得出了THFB梁的承载力随不同参数的变化规律。最后结合理论和有限元分析,验证了Eurocode 3提供的H型钢梁设计公式计算THFB极限承载力的适用性。研究结果表明:采用Eurocode 3提供的H型钢梁设计公式对THFB的极限承载力进行验算是安全的,但偏于保守。 展开更多
关键词 三角形缘梁 承载力 试验 有限元分析
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小展弦比超音速飞机机翼气动特性分析
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作者 赵蓉 刘旭辉 孙瑜珮 《成都航空职业技术学院学报》 2021年第1期42-45,共4页
基于采用对称翼型的小展弦比三角形机翼模型,对其在亚音速状态和超音速状态时的升力特性、阻力特性、升阻比特性、稳定性特性进行了理论计算分析。并针对该模型进行数值模拟,分析其超音速流场特性,与理论分析结果进行对比,发现相差不大... 基于采用对称翼型的小展弦比三角形机翼模型,对其在亚音速状态和超音速状态时的升力特性、阻力特性、升阻比特性、稳定性特性进行了理论计算分析。并针对该模型进行数值模拟,分析其超音速流场特性,与理论分析结果进行对比,发现相差不大。得出结论:该翼型机翼在飞机巡航速度为Ma=2时气动性能较好。 展开更多
关键词 小展弦比 三角形翼 超音速飞机 数值模拟
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Convective mass transfer enhancement in a membrane channel by delta winglets and their comparison with rectangular winglets
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作者 闵敬春 张冰强 《Chinese Journal of Chemical Engineering》 SCIE EI CAS CSCD 2015年第11期1755-1762,共8页
Numerical calculations were conducted to simulate the flow and mass transfer in narrow membrane channels equipped with delta winglets, which are often used as longitudinal vortex generators to enhance heat transfer in... Numerical calculations were conducted to simulate the flow and mass transfer in narrow membrane channels equipped with delta winglets, which are often used as longitudinal vortex generators to enhance heat transfer in heat exchanger applications. The channel consists of an impermeable solid wall and a membrane. The delta winglets are attached to the solid wall surface to enhance the mass transfer near the membrane surface and suppress the concentration polarization. The winglet performance was evaluated in terms of concentration polarization factor versus consumed pumping power. Calculations were implemented for NaCl solution flow in a membrane channel having a height of 2.0 mm for Reynolds numbers ranging from 400 to 1000. The delta wing- lets were optimized under equal pumping power condition, and the results of optimization suggest winglet height of 5/6 of the channel height, aspect ratio of 2.0, attack angle of 30% and a winglet interval equal to the channel height The optimal delta winglets were compared with the optimal rectangular winglets we found previously, and it is shown that the rectangular winglets yield a somewhat better performance than the delta winglets. @ 2015 The Chemical Industry and Engineering Society of China, and Chemical Industry Press. All rights reserved. 展开更多
关键词 Membrane processConcentration polarizationMass transfer enhancementDelta wingletPumping power
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