Zobrazit minimální záznam



dc.contributor.authorČervinka , Jan
dc.contributor.authorKulhánek , Robert
dc.contributor.authorPátek , Zdeněk
dc.date.accessioned2017-10-03T07:32:12Z
dc.date.available2017-10-03T07:32:12Z
dc.date.issued2017
dc.identifier.citationActa Polytechnica. 2017, vol. 57, no. 1, p. 1-7.
dc.identifier.issn1210-2709 (print)
dc.identifier.issn1805-2363 (online)
dc.identifier.urihttp://hdl.handle.net/10467/72690
dc.description.abstractThe significance of the influence of operating propellers on the aircraft aerodynamic characteristics is well-known. Wind tunnel testing of an airplane model with operating propellers is a complex task regarding the required similarity of the full-scale and the model case. Matching sufficient similarity in axial and rotational velocities in the propeller slipstream is the primordial condition for the global aerodynamic similarity of the windtunnel testing. An example of the model power units with related devices is presented. Examples of the wind tunnel testing results illustrate the extent of the propeller influence on aerodynamic characteristics of an aircraft of unconventional configuration with power units positioned at the fuselage afterbody.en
dc.format.mimetypeapplication/pdf
dc.language.isoeng
dc.publisherČeské vysoké učení technické v Prazecs
dc.publisherCzech Technical University in Pragueen
dc.relation.ispartofseriesActa Polytechnica
dc.relation.urihttps://ojs.cvut.cz/ojs/index.php/ap/article/view/3756
dc.rightsCreative Commons Attribution 4.0 International Licenseen
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/
dc.subjectwindtunnel testing, propeller slipstream, T-tail aircraft, propeller simulationen
dc.titleAN AIRPLANE WITH UNCONVENTIONALLY PLACED PROPELLER POWER UNIT
dc.typearticleen
dc.date.updated2017-10-03T07:32:12Z
dc.identifier.doi10.14311/AP.2017.57.0001
dc.rights.accessopenAccess
dc.type.statusPeer-reviewed
dc.type.versionpublishedVersion


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Zobrazit minimální záznam

Creative Commons Attribution 4.0 International License
Kromě případů, kde je uvedeno jinak, licence tohoto záznamu je Creative Commons Attribution 4.0 International License