Silva, PauloTsoutsanis, Panagiotis2024-06-122024-06-122022-02-09Silva, Paulo; Tsoutsanis, Panagiotis (2022). Data supporting 'Numerical Investigation of full helicopter with and without the ground effect'. Cranfield Online Research Data (CORD). Dataset. https://doi.org/10.17862/cranfield.rd.19146182https://dspace.lib.cranfield.ac.uk/handle/1826/22473In the present work, the aerodynamic performance of the full helicopter PSP in hover flight is investigated using a simplified concept of multiple reference frame (MRF) technique in the context of high-order Monotone Upstream Centred Scheme for Conservation Laws (MUSCL) cell-centred finite volume method. The predictions were obtained for two ground distances and several collective pitch angle at tip Mach number of 0.585. The calculations were made for both out-of-ground-effect (OGE) and in-ground-effect (IGE) cases and compared with experimental data in terms of pressure distribution and integrated thrust and torque and vortex system.CC BY 4.0https://creativecommons.org/licenses/by/4.0/Full helicopter''CFD''PSP''Ground Effect''Pressure distribuition'Dataset10.17862/cranfield.rd.19146182