Assessment of Detached Eddy Simulation and Sliding Mesh Interface in Predicting Tiltrotor Performance in Helicopter and Airplane Modes
Fluid Dynamics
2022-01-28 v1
Abstract
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.
Keywords
Cite
@article{arxiv.2201.11560,
title = {Assessment of Detached Eddy Simulation and Sliding Mesh Interface in Predicting Tiltrotor Performance in Helicopter and Airplane Modes},
author = {Feilin Jia and John Moore and Qiqi Wang},
journal= {arXiv preprint arXiv:2201.11560},
year = {2022}
}