Počet záznamů: 1
Reduced modelling of aeroelastic instability in a turbine blade cascade
- 1.0573341 - ÚT 2024 CZ eng C - Konferenční příspěvek (zahraniční konf.)
Pešek, Luděk - Šnábl, Pavel - Prasad, Chandra Shekhar
Reduced modelling of aeroelastic instability in a turbine blade cascade.
Dynamics of Machines and Mechanical Systems with Interactions : DYMAMESI 2023. Prague: Institute of Thermomechanics of the CAS, v. v. i., 2023 - (Zolotarev, I.; Pešek, L.; Kozień, M.), s. 59-64. ISBN 978-80-87012-85-7.
[DYMAMESI 2023. Cracow - Prague (PL), 28.02.2023-01.03.2023]
Grant CEP: GA ČR(CZ) GA20-26779S
Institucionální podpora: RVO:61388998
Klíčová slova: flutter * blade cascade * self-excitation * Van der Pol
Obor OECD: Mechanical engineering
The contribution deals with the first results on flutter instability of the linear cascade triggered by impulse excitation. Together with experimental results, numerical results obtained by reduced modelling of the cascade using van der Pol model of self-excitation are presented and discussed.
Trvalý link: https://hdl.handle.net/11104/0350046
Počet záznamů: 1