Simulation of a maneuvering aircraft using a panel method

Simple item page
dc.contributor.authorSchoř, Pavelcs
dc.contributor.authorKouřil, Martincs
dc.contributor.authorDaněk, Vladimírcs
dc.coverage.issue2cs
dc.coverage.volume61cs
dc.date.accessioned2022-04-25T10:54:05Z
dc.date.available2022-04-25T10:54:05Z
dc.date.issued2021-04-30cs
dc.description.abstractWe present a method for numerical simulations of a maneuvering aircraft, which uses a first-order unsteady panel method as the only source of aerodynamic forces and moments. By using the proposed method, it is possible to simulate a motion of an aircraft, while the only required inputs are geometry and inertia characteristics, which significantly reduces the time required to start the simulation. We validated the method by a comparison of recordings of flight parameters (position, velocities, accelerations) from an actual acrobatic flight of a glider and the results obtained from the simulations. The simulation was controlled by deflections of control surfaces recorded during the actual flight. We found a reasonable agreement between the experimental data and the simulation. The design of our method allows to evaluate not only the integral kinematic quantities but also instant local pressure and inertia loads. This makes our method useful also for a load evaluation of an aircraft. A significant advantage of the proposed method is that only an ordinary workstation computer is required to perform the simulation.en
dc.formattextcs
dc.format.extent378-390cs
dc.format.mimetypeapplication/pdfcs
dc.identifier.citationActa Polytechnica. 2021, vol. 61, issue 2, p. 378-390.en
dc.identifier.doi10.14311/AP.2021.61.0378cs
dc.identifier.issn1210-2709cs
dc.identifier.other176868cs
dc.identifier.urihttp://hdl.handle.net/11012/204106
dc.language.isoencs
dc.publisherCzech Technical University in Praguecs
dc.relation.ispartofActa Polytechnicacs
dc.relation.urihttps://ojs.cvut.cz/ojs/index.php/ap/article/view/6627cs
dc.rightsCreative Commons Attribution 4.0 Internationalcs
dc.rights.accessopenAccesscs
dc.rights.sherpahttp://www.sherpa.ac.uk/romeo/issn/1210-2709/cs
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/cs
dc.subjectFlight Mechanicsen
dc.subjectAerodynamicsen
dc.subjectSimulationen
dc.subjectPanel methoden
dc.subjectManeuvering Aircraften
dc.titleSimulation of a maneuvering aircraft using a panel methoden
dc.type.driverarticleen
dc.type.statusPeer-revieweden
dc.type.versionpublishedVersionen
sync.item.dbidVAV-176868en
sync.item.dbtypeVAVen
sync.item.insts2023.03.01 12:53:07en
sync.item.modts2023.03.01 12:14:33en
thesis.grantorVysoké učení technické v Brně. Fakulta strojního inženýrství. Letecký ústavcs
thesis.grantorVysoké učení technické v Brně. . AeroMobil R&D, s. r. o.cs
Files
Original bundle
Now showing 1 - 1 of 1
Thumbnail Image
Name:
document2.pdf
Size:
4.86 MB
Format:
Adobe Portable Document Format
Description:
document2.pdf
Download
Collections
Letecký ústav