论文标题
在预测直升机和飞机模式中的横架性能中评估独立的涡流模拟和滑动网格界面
Assessment of Detached Eddy Simulation and Sliding Mesh Interface in Predicting Tiltrotor Performance in Helicopter and Airplane Modes
论文作者
论文摘要
本文介绍了在直升机模式下（悬停飞行和向前飞行）和飞机螺旋桨模式的全尺度XV-15 tiltrotor的性能和流场的数值研究，其中使用独立的涡流模拟，其中转子的移动是使用滑动网格界面来实现的。进行CFD结果与实验数据和其他CFD结果的比较。
This paper presents numerical investigation on performance and flow field of the full-scale XV-15 tiltrotor in both helicopter mode (hovering flight and forward flight) and aeroplane propeller mode using Detached Eddy Simulation, in which the movement of the rotor is achieved using a Sliding Mesh Interface. Comparison of our CFD results against experiment data and other CFD results is performed and presented.
