Numerical investigation of full helicopter with and without the ground effect

Simple item page
dc.contributor.authorSilva, Paulo A. S. F.
dc.contributor.authorTsoutsanis, Panagiotis
dc.contributor.authorAntoniadis, Antonis F.
dc.date.accessioned2022-02-24T15:51:16Z
dc.date.available2022-02-24T15:51:16Z
dc.date.issued2022-02-15
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.en_UK
dc.identifier.citationSilva PASF, Tsoutsanis P, Antoniadis AF. (2022) Numerical Investigation of full helicopter with and without the ground effect, Aerospace Science and Technology, Volume 122, Issue March, Article number 107401en_UK
dc.identifier.issn1270-9638
dc.identifier.urihttps://doi.org/10.1016/j.ast.2022.107401
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/17598
dc.language.isoenen_UK
dc.publisherElsevieren_UK
dc.rightsAttribution 4.0 International*
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/*
dc.subjectHigh-order methodsen_UK
dc.subjectRotorcraften_UK
dc.subjectCFDen_UK
dc.subjectIGEen_UK
dc.subjectOGEen_UK
dc.subjectGround effecten_UK
dc.titleNumerical investigation of full helicopter with and without the ground effecten_UK
dc.typeArticleen_UK

Files

Original bundle
Now showing 1 - 1 of 1
Thumbnail Image
Name:
Numerical_investigation_of_full_helicopter-2022.pdf
Size:
2.76 MB
Format:
Adobe Portable Document Format
Description:
Download
License bundle
Now showing 1 - 1 of 1
No Thumbnail Available
Name:
license.txt
Size:
1.63 KB
Format:
Item-specific license agreed upon to submission
Description:
Download

Collections

Staff publications (SATM)