Full metadata record
| DC pole | Hodnota | Jazyk |
|---|---|---|
| dc.contributor.author | Narovec, Jan | |
| dc.contributor.author | Duda, Daniel | |
| dc.contributor.author | Horáček, Vít | |
| dc.contributor.author | Tomášková, Tetjana | |
| dc.contributor.author | Uruba, Václav | |
| dc.contributor.author | Yanovych, Vitalii | |
| dc.date.accessioned | 2023-03-20T11:00:16Z | - |
| dc.date.available | 2023-03-20T11:00:16Z | - |
| dc.date.issued | 2022 | |
| dc.identifier.citation | NAROVEC, J. DUDA, D. HORÁČEK, V. TOMÁŠKOVÁ, T. URUBA, V. YANOVYCH, V. Vorticity statistics in the near wake of asymmetric prismatic airfoil NACA 64-618 at negative angle of attack –10° at Reynolds numbers 1.6 ⋅ 104 and 1.6 ⋅ 105 in distance 0.0 – 0.4 × chord past trailing edge measured by Particle Image Velocimetry. In MATEC Web of Conferences Volume 367 (2022) 21st Conference on Power System Engineering. Plzeň: EPD Sciences, 2022. s. nestránkováno. ISBN: neuvedeno , ISSN: 2261-236X | cs |
| dc.identifier.issn | 2261-236X | |
| dc.identifier.uri | http://hdl.handle.net/11025/51720 | |
| dc.format | 8 s. | cs |
| dc.format.mimetype | application/pdf | |
| dc.language.iso | en | en |
| dc.publisher | EPD Sciences | en |
| dc.relation.ispartofseries | MATEC Web of Conferences Volume 367 (2022) 21st Conference on Power System Engineering | en |
| dc.rights | © CC BY-NC-ND 4.0 | en |
| dc.title | Vorticity statistics in the near wake of asymmetric prismatic airfoil NACA 64-618 at negative angle of attack –10° at Reynolds numbers 1.6 ⋅ 104 and 1.6 ⋅ 105 in distance 0.0 – 0.4 × chord past trailing edge measured by Particle Image Velocimetry | en |
| dc.type | konferenční příspěvek | cs |
| dc.type | ConferenceObject | en |
| dc.rights.access | openAccess | en |
| dc.type.version | publishedVersion | en |
| dc.description.abstract-translated | The airfoil NACA 64-618 is realized by using two levels of quality: first the theoretical profile is printed on a 3D printer in a direct, “naive” way, this geometry has been scanned by using 3D scanner and based on the deviations, a better model has been processed. The flow within the turbulent wake is measured by using Particle Image Velocimetry (PIV) technique at two velocities separated by one order of magnitude | en |
| dc.subject.translated | Vorticity | en |
| dc.subject.translated | Particle Imag Velocimetry | en |
| dc.subject.translated | Turbulence | en |
| dc.subject.translated | Airfoil | en |
| dc.subject.translated | NACA64-618 | en |
| dc.subject.translated | Manufacturing Inaccuracies | en |
| dc.identifier.doi | 10.1051/matecconf/202236700017 | |
| dc.type.status | Peer-reviewed | en |
| dc.identifier.obd | 43936973 | |
| dc.project.ID | EF16_026/0008389/LoStr: Výzkumná spolupráce pro dosažení vyšší účinnosti a spolehlivosti lopatkových strojů | cs |
| Vyskytuje se v kolekcích: | Konferenční příspěvky / Conference papers (KKE) OBD | |
Soubory připojené k záznamu:
| Soubor | Velikost | Formát | |
|---|---|---|---|
| matecconf_pse22_00017-(NACA64-618-PSE2022).pdf | 1,66 MB | Adobe PDF | Zobrazit/otevřít |
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