Navier‐Stokes computational fluid dynamics calculations are presented for isolated, half‐
span, and full‐span V‐22 tiltrotor hover configurations. These computational results extend …

Multicopter drones have a complex geometry involving several rotors. Therefore,
computational resources could hinder their aeroacoustics modelling and simulation …

Swarms of drones is an emerging field of research and technology. Multicopter drones are
noisy machines, and the noise effects would increase for a swarm. It is, therefore, essential …

采用试验方法测量了悬停和过渡状态倾转旋翼机旋翼/机翼气动干扰特性,
部分揭示了干扰流动的机理. 基于3D-PIV (particle image velocimetry) 技术的流场测量结果 …

Rotorcraft brownout is caused by the entrainment of dust and sand particles in helicopter
downwash, resulting in reduced pilot visibility during low, slow flight and landing. Recently …

In order to calculate the unsteady aerodynamic characteristics of a tilt-rotor in a conversion
mode, a virtual blade model (VBM) and an real blade model (RBM) are established …

针对倾转旋翼存在直升机和固定翼两种工作模式特点, 将CFD 方法与优化方法相结合,
建立了一套倾转旋翼/螺旋桨气动外形综合优化设计方法. 首先, 发展了一套适合桨叶气动外形 …

This report documents the development of a computational model to simulate the complex
flow induced by helicopter rotors, using an open-source computational fluid dynamics CFD …

For physically realistic rotor systems, integrated performance in hover and near-hover (low
speed or low wind) conditions depends critically on rotor/airframe interaction, specifically the …

This work investigates important aeromechanics phenomena affecting the V-22 tilt rotor in
low speed sideward flight or while hovering in quartering or crosswind conditions. These …