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基于CFX的风机阵模拟甘蔗田间边界层风速研究
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作者 郭无极 袁俊杰 《装备制造技术》 2018年第11期99-102,114,共5页
旨在研究一种能够模拟甘蔗田间风速的风机阵。针对这一目的,首先研究了轴流风机风场的模拟方法,并通过物理试验对该方法进行了验证。再使用该方法对交错排布和平行排布两种不同排布方式的风机阵进行了仿真。分析对比发现,两种方法都可... 旨在研究一种能够模拟甘蔗田间风速的风机阵。针对这一目的,首先研究了轴流风机风场的模拟方法,并通过物理试验对该方法进行了验证。再使用该方法对交错排布和平行排布两种不同排布方式的风机阵进行了仿真。分析对比发现,两种方法都可以较好的模拟出近地面满足指数率的风场。 展开更多
关键词 轴流风机 CFD 风机阵 边界层风速
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DESIGN AND IMPLEMENTATION OF GUST RESPONSEALLEVIATION CONTROL SYSTEM FOR HELICOPTERS 被引量:1
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作者 龚华军 杨一栋 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2004年第1期13-17,共5页
Gust response alleviation is very important for helicopters which have strong coupling and vibration. Gust disturbance not only influences the ride quality and the precision of the weapon delivery, but also affects to... Gust response alleviation is very important for helicopters which have strong coupling and vibration. Gust disturbance not only influences the ride quality and the precision of the weapon delivery, but also affects to the structural fatigue load and the strength. The method of an optimal control law to suppress the gust disturbance for helicopters is presented. The optimization requires the minimization of the vertical overload at the pilot′s seat, the attitude variation and the control energy consumption under the gust disturbance. Based on the original control system, the new system can be easily realized by adding a vertical speed feedback passage. In order to develop the real-time operational flight control system, the optimized control law is written in C language. The hybrid simulations prove that the performance of gust response alleviation and the efficiency of digitalization are satisfactory. 展开更多
关键词 HELICOPTER gust response optimal control flight control
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