Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/146639
Full metadata record
DC FieldValueLanguage
dc.contributor.authorNathanael, Joshua C.en_US
dc.contributor.authorWang, John Chung-Hungen_US
dc.contributor.authorLow, Kin Huaten_US
dc.date.accessioned2021-03-04T01:43:14Z-
dc.date.available2021-03-04T01:43:14Z-
dc.date.issued2021-
dc.identifier.citationNathanael, J. C., Wang, J. C.-H., & Low, K. H. (2021). Preliminary investigation of wake vortex generated by spinning quadrotor propellers using overset mesh. Proceedings of the AIAA SciTech 2021 Forum. doi:10.2514/6.2021-1309en_US
dc.identifier.isbn978-1-62410-609-5-
dc.identifier.urihttps://hdl.handle.net/10356/146639-
dc.description.abstractAs unmanned aircraft or drones are becoming more commonplace in our ever-developing environment where a number of drones can be flying in the same given airspace, a drone is likely to experience wake vortex turbulence from another drone nearby. Therefore, there is a need to understand how the airflow is generated from one vehicle and to what extent this airflow might affect another vehicle. Results of such studies will be useful in the establishment of safe separation for drone operations. In the present work, flow simulations are carried out using overset mesh on ANSYS Fluent 19.2 for both single and multiple propellers, and the flights in hovering and forwarding motion are considered. The simulation results obtained are in general agreement with the simulation and experimental results that are available from other studies. This provides support to the idea that the method of flow simulation can be acceptably reliable in predicting the resulting airflow from a flying drone and the proposed method can be further applied to various cases of drone flights.en_US
dc.description.sponsorshipCivil Aviation Authority of Singapore (CAAS)en_US
dc.language.isoenen_US
dc.rights© 2021 Nanyang Technological University. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission.en_US
dc.subjectEngineering::Aeronautical engineering::Aerodynamicsen_US
dc.subjectEngineering::Aeronautical engineering::Aviationen_US
dc.titlePreliminary investigation of wake vortex generated by spinning quadrotor propellers using overset meshen_US
dc.typeConference Paperen
dc.contributor.conferenceAIAA SciTech 2021 Forumen_US
dc.contributor.researchAir Traffic Management Research Instituteen_US
dc.identifier.doi10.2514/6.2021-1309-
dc.description.versionAccepted versionen_US
dc.subject.keywordsDronesen_US
dc.subject.keywordsWake Vortexen_US
dc.description.acknowledgementThe authors would like to thank the Air Traffic Management Research Institute (ATMRI) for funding this research under the UAS Programme.en_US
item.grantfulltextopen-
item.fulltextWith Fulltext-
Appears in Collections:ATMRI Conference Papers

Page view(s)

47
Updated on May 15, 2021

Download(s)

18
Updated on May 15, 2021

Google ScholarTM

Check

Altmetric


Plumx

Items in DR-NTU are protected by copyright, with all rights reserved, unless otherwise indicated.