CERESResearch Repository

UCNS3d MRF testcases

dc.contributor.authorSilva, Paulo
dc.contributor.authorTsoutsanis, Panagiotis
dc.date.accessioned2026-04-09T05:55:15Z
dc.date.available2026-04-09T05:55:15Z
dc.date.issued2023-10-31 16:09
dc.description.abstractThis repository contains the Grids used as tescase on the UCNS3d for four helicopter cases: * Caradonna and Tung (out of ground effect): The mesh files and results of the test case from section 4 used on the publication ["Hovering rotor solutions by high-order methods on unstructured grids"](https://doi.org/10.1016/j.ast.2019.105648) * Paint Sensitive Pressure rotor (out of ground effect): The periodic mesh files and results of the test case from section 5 used on the publication ["Hovering rotor solutions by high-order methods on unstructured grids"](https://doi.org/10.1016/j.ast.2019.105648) * Black Hawk 'UH-60a' (out of ground effect): The periodic mesh files and results of the test case from section 6 used on the publication ["Hovering rotor solutions by high-order methods on unstructured grids"](https://doi.org/10.1016/j.ast.2019.105648) * Caradonna and Tung (with and without ground effect): The mesh files and results of the test case used on the publication ["Simple multiple reference frame for high-order solution of hovering rotors with and without ground effect"](https://doi.org/10.1016/j.ast.2021.106518) * S-76 (with and without ground effect): The mesh files and results of the test case used on the publication ["Simple multiple reference frame for high-order solution of hovering rotors with and without ground effect"](https://doi.org/10.1016/j.ast.2021.106518) * Paint Sensitive Pressure full-helicopter (with and without ground effect): The periodic mesh files and results of the test case from section 5 used on the publication ["Numerical Investigation of full helicopter with and without the ground effect"](https://doi.org/10.1016/j.ast.2022.107401 and the Data underlying this study can be accessed through the [Cranfield University repository](https://doi.org/10.17862/cranfield.rd.19146182.v1). For this study we used the surface unstructured Blade grid downloaded at (https://www.aiaa-hpw.org/psp-rotor) and the robin fuselage geometry downloaded at (https://github.com/Applied-Scientific-Research/robin-surface-mesh) which changes accordingly to the mod7 geometry as exposed at (https://ntrs.nasa.gov/citations/20100033120).
dc.identifier.citationSilva, Paulo; Tsoutsanis, Panagiotis (2023). UCNS3d MRF testcases. Cranfield Online Research Data (CORD). Dataset. https://doi.org/10.17862/cranfield.rd.24271132
dc.identifier.doi10.17862/cranfield.rd.24271132
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/25139
dc.identifier.urihttps://doi.org/10.17862/cranfield.rd.24271132
dc.publisherCranfield University
dc.rightsCC BY 4.0
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/
dc.subject'UCNS3D'
dc.subject'Rotor'
dc.subject'Helicopters'
dc.subject'CFD'
dc.titleUCNS3d MRF testcases
dc.typeDataset

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