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0510198 - ÚT 2020 GR eng C - Conference Paper (international conference)
Prasad, Chandra Shekhar - Pešek, Luděk
A hybrid incompressible boundary element based reduced ordered aeroelastic model for fast aeroelstic simulations for flexible wing and turbomachinery blade cascade.
ICOVP 2019. Atény: National Technical University of Athens, 2019 - (Sapountzakis, E.), s. 1-13
[ICOVP 2019. Kréta (GR), 01.09.2019-04.09.2019]
Institutional support: RVO:61388998
Keywords : turbomachinery * dynamic stall flutter * boundary layer method * reduce order aeroelastic mode * blade cascade
OECD category: Applied mechanics
Permanent Link: http://hdl.handle.net/11104/0302582