Data supporting 'Numerical Investigation of full helicopter with and without the ground effect'

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dc.contributor.authorSilva, Paulo
dc.contributor.authorTsoutsanis, Panagiotis
dc.date.accessioned2024-06-12T12:56:59Z
dc.date.available2024-06-12T12:56:59Z
dc.date.issued2022-02-09 18:11
dc.description.abstractIn 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.
dc.description.sponsorshipPeta-5: A National Facility for Petascale Data Intensive Computation and Analytics
dc.identifier.citationSilva, 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.19146182
dc.identifier.doi10.17862/cranfield.rd.19146182
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/22473
dc.publisherCranfield University
dc.relation.supplementshttps://doi.org/10.1016/j.ast.2022.107401'
dc.rightsCC BY 4.0
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/
dc.subjectFull helicopter'
dc.subject'CFD'
dc.subject'PSP'
dc.subject'Ground Effect'
dc.subject'Pressure distribuition'
dc.titleData supporting 'Numerical Investigation of full helicopter with and without the ground effect'
dc.typeDataset

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