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Effect of Initial Pitching Angle on Helicopter Ditching Characteristics Using Smoothed-Particle-Hydrodynamics Method
Journal of Aircraft ( IF 2.2 ) Pub Date : 2021-01-01 , DOI: 10.2514/1.c035898 Tianhang Xiao 1 , Zhaoyan Lu 1 , Shuanghou Deng 1
Journal of Aircraft ( IF 2.2 ) Pub Date : 2021-01-01 , DOI: 10.2514/1.c035898 Tianhang Xiao 1 , Zhaoyan Lu 1 , Shuanghou Deng 1
Affiliation
The present Paper investigates the ditching characteristics of a helicopter model by means of an in-house-developed smoothed-particle-hydrodynamics solver coupled with a six degree-of-freedom motio...
中文翻译：
使用平滑粒子流体动力学方法研究初始俯仰角对直升机开沟特性的影响
本论文通过内部开发的平滑粒子流体动力学求解器和六自由度运动...
更新日期：2021-01-01
中文翻译：
使用平滑粒子流体动力学方法研究初始俯仰角对直升机开沟特性的影响
本论文通过内部开发的平滑粒子流体动力学求解器和六自由度运动...
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