平底直升机着水载荷和压力分布估算方法研究 |
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引用本文: | 马玉杰,汪正中,陈立霞.平底直升机着水载荷和压力分布估算方法研究[J].直升机技术,2014(1):1-5. |
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作者姓名: | 马玉杰 汪正中 陈立霞 |
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作者单位: | 中国直升机设计研究所,直升机旋翼动力学重点实验室,江西景德镇333001 |
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摘 要: | 将平底直升机底部形状简化为一矩形平板,基于经典的水动力冲击理论,建立简化的刚体运动方程,对其求解得到着水载荷及压力分布的估算方法。计算结果与国外相关资料比较,其准确性可以满足实际工程的要求。
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关 键 词: | 平底直升机 着水载荷 压力分布 平板 |
Estimation of Impact Loads and Pressure Distribution of a Flat-Plate Helicopter |
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Authors: | MA Yujie WANG Zhengzhong CHEN Lixia |
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Institution: | (National Key Laboratory of Rotorcraft Aeromechanics, CHRDI, Jingdezhen Jiangxi, 333001 ) |
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Abstract: | The helicopter bottom shape was simplified as a rectangular plate. Based on the classical hydrodynamic impact theory, the simplified rigid motion equations were established, and the estima- tion of impcat loads and pressure distribution were developed. The results were compared with for- eign references, and the accuracy could satisfy the requirements of engineering. |
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Keywords: | helicopter impact loads pressure distribution flat-plate |
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