Numerical Modelling of Hypersonic Flow of Spacecrafts
but.event.date | 26.04.2022 | cs |
but.event.title | STUDENT EEICT 2022 | cs |
dc.contributor.author | Mačák, Martin | |
dc.contributor.author | Vyroubal, Petr | |
dc.date.accessioned | 2022-12-06T13:22:00Z | |
dc.date.available | 2022-12-06T13:22:00Z | |
dc.date.issued | 2022 | cs |
dc.description.abstract | Numerical simulations of rarefied gas flows are an important area in the design of aerospace vehicles. They can provide a suitable alternative to experiments, which can be often too complicated due to extreme conditions. Navier-Stokes equations, which describe continuum fluid flow, generally lose their applicability in low pressures. As a result, it is necessary to adjust these equations or use alternative models. This article studies the possibility of using a continuum numerical model for a simulation of a hypersonic flow of a reentry module. Based on the Knudsen number, it was shown that it is still possible to use Navier-Stokes equations either without any adjustments or with the addition of a slip flow boundary condition. | en |
dc.format | text | cs |
dc.format.extent | 238-242 | cs |
dc.format.mimetype | application/pdf | en |
dc.identifier.citation | Proceedings II of the 28st Conference STUDENT EEICT 2022: Selected papers. s. 238-242. ISBN 978-80-214-6030-0 | cs |
dc.identifier.doi | 10.13164/eeict.2022.238 | |
dc.identifier.isbn | 978-80-214-6030-0 | |
dc.identifier.uri | http://hdl.handle.net/11012/208644 | |
dc.language.iso | en | cs |
dc.publisher | Vysoké učení technické v Brně, Fakulta elektrotechniky a komunikačních technologií | cs |
dc.relation.ispartof | Proceedings II of the 28st Conference STUDENT EEICT 2022: Selected papers | en |
dc.relation.uri | https://conf.feec.vutbr.cz/eeict/index/pages/view/ke_stazeni | cs |
dc.rights | © Vysoké učení technické v Brně, Fakulta elektrotechniky a komunikačních technologií | cs |
dc.rights.access | openAccess | en |
dc.subject | rarefied flow, Knudsen number, Ansys Fluent, hypersonic flow, spacecraft | en |
dc.title | Numerical Modelling of Hypersonic Flow of Spacecrafts | en |
dc.type.driver | conferenceObject | en |
dc.type.status | Peer-reviewed | en |
dc.type.version | publishedVersion | en |
eprints.affiliatedInstitution.department | Fakulta elektrotechniky a komunikačních technologií | cs |
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