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
Authors:	Narovec, Jan Duda, Daniel Horáček, Vít Tomášková, Tetjana Uruba, Václav Yanovych, Vitalii
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
Issue Date:	2022
Publisher:	EPD Sciences
Document type:	konferenční příspěvek ConferenceObject
URI:	http://hdl.handle.net/11025/51720
ISSN:	2261-236X
Keywords in different language:	Vorticity;Particle Imag Velocimetry;Turbulence;Airfoil;NACA64-618;Manufacturing Inaccuracies
Abstract in different language:	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
Rights:	© CC BY-NC-ND 4.0
Appears in Collections:	Konferenční příspěvky / Conference papers (KKE) OBD

Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.