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平底直升机着水载荷和压力分布估算方法研究
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.
作者姓名:马玉杰  汪正中  陈立霞
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
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。

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
Authors:MA Yujie  WANG Zhengzhong  CHEN Lixia
Institution:(National Key Laboratory of Rotorcraft Aeromechanics, CHRDI, Jingdezhen Jiangxi, 333001 )
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.
Keywords:helicopter  impact loads  pressure distribution  flat-plate
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