Vis enkel innførsel

dc.contributor.authorMuhammed, Manaf
dc.contributor.authorVirk, Muhammad Shakeel
dc.date.accessioned2023-08-17T09:44:27Z
dc.date.available2023-08-17T09:44:27Z
dc.date.issued2023-03-08
dc.description.abstractIce accretion on rotary-wing unmanned aerial vehicles (RWUAVs) needs to be studied separately from the fixed-wing UAVs because of the additional flow complexities induced by the propeller rotation. The aerodynamics of rotatory wings are extremely challenging compared to the fixed-wing configuration. Atmospheric icing can be considered a hazard that can plague the operation of UAVs, especially in the Arctic region, as it can impose severe aerodynamic penalties on the performance of propellers. Rotary-wing structures are more prone to ice accretion and ice shedding because of the centrifugal force due to rotational motion, whereby the shedding of the ice can lead to mass imbalance and vibration. The nature of ice accretion on rotatory wings and associated performance degradation need to be understood in detail to aid in the optimum design of rotary-wing UAVs, as well as to develop adequate ice mitigation techniques. Limited research studies are available about icing on rotary wings, and no mature ice mitigation technique exists. Currently, there is an increasing interest in research on these topics. This paper provides a comprehensive review of studies related to icing on RWUAVs, and potential knowledge gaps are also identified.en_US
dc.identifier.citationMuhammed M, Virk MS. Ice Accretion on Rotary-Wing Unmanned Aerial Vehicles—A Review Study. Aerospace. 2023;10(3), 261en_US
dc.identifier.cristinIDFRIDAID 2132362
dc.identifier.doi10.3390/aerospace10030261
dc.identifier.issn2226-4310
dc.identifier.urihttps://hdl.handle.net/10037/30034
dc.language.isoengen_US
dc.publisherMDPIen_US
dc.relation.journalAerospace
dc.rights.accessRightsopenAccessen_US
dc.rights.holderCopyright 2023 The Author(s)en_US
dc.rights.urihttps://creativecommons.org/licenses/by/4.0en_US
dc.rightsAttribution 4.0 International (CC BY 4.0)en_US
dc.titleIce Accretion on Rotary-Wing Unmanned Aerial Vehicles—A Review Studyen_US
dc.type.versionpublishedVersionen_US
dc.typeJournal articleen_US
dc.typeTidsskriftartikkelen_US
dc.typePeer revieweden_US


Tilhørende fil(er)

Thumbnail

Denne innførselen finnes i følgende samling(er)

Vis enkel innførsel

Attribution 4.0 International (CC BY 4.0)
Med mindre det står noe annet, er denne innførselens lisens beskrevet som Attribution 4.0 International (CC BY 4.0)