Original title: EXPERIMENTAL BLADE CASCADE FOR AEROELASTIC STUDIES IN THE PRESENCE OF 3D FLOW STRUCTURES: INITIAL DESIGN IDEA
Authors: Šnábl, Pavel ; Prasad, Chandra Shekhar ; Pešek, Luděk ; Procházka, Pavel P.
Document type: Papers
Conference/Event: International Colloquium DYMAMESI 2024, Prague (CZ), 20240305
Year: 2024
Language: eng
Abstract: In order to study the aeroelasticity in a blade cascade experimentally, simplifications must be made to make any measurements possible. Therefore, most researchers use linear cascades: parallel blades with constant cross-sections which essentially reduce the problem to 2D. Although linear cascades lack some key features such as rotational periodicity and the radial flow component, it is still possible to obtain and study aeroelastic couplings. The aim of the experimental cascade presented in this paper is to include the radial flow component by creating a bypass flow loop on the wind tunnel and having deformable blades fixed on one side only. When such blades oscillate, the channel width between the blades changes unevenly along the blade span. This experimental setup allows the effect of 3D flow in a blade cascade to be studied.\n
Keywords: 3D flow structures; aeroelasticity; blade cascade; experiment
Host item entry: Dynamics of Machines and Mechanical Systems with Interactions : DYMAMESI 2024, ISBN 978-80-87012-89-5

Institution: Institute of Thermomechanics AS ČR (web)
Document availability information: Fulltext is available at the institute of the Academy of Sciences.
Original record: https://hdl.handle.net/11104/0358056

Permalink: http://www.nusl.cz/ntk/nusl-668298


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