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0535111 - ÚT 2021 RIV GR eng C - Konferenční příspěvek (zahraniční konf.)
Prasad, Chandra Shekhar - Pešek, Luděk
Subsonic stall flutter analysis in 2D blade cascade using hybrid boundary element method.
EURODYN 2020. Vol. 1. Athens: National Technical University of Athens (NTUA), 2020 - (Papadrakakis, M.; Fragiadakis, M.; Papadimitriou, C.), s. 213-224. ISBN 978-618-85072-0-3.
[EURODYN 2020 /11./. Athény (GR), 23.11.2020-26.11.2020]
Grant CEP: GA TA ČR(CZ) TN01000007
Institucionální podpora: RVO:61388998
Klíčová slova: stall flutter * aeroelasticity * boundary element method * discrete vortex particle method * panel method * blade cascade * Viscous-inviscid coupling
Obor OECD: Applied mechanics
Trvalý link: http://hdl.handle.net/11104/0315414
Prasad, Chandra Shekhar - Pešek, Luděk
Subsonic stall flutter analysis in 2D blade cascade using hybrid boundary element method.
EURODYN 2020. Vol. 1. Athens: National Technical University of Athens (NTUA), 2020 - (Papadrakakis, M.; Fragiadakis, M.; Papadimitriou, C.), s. 213-224. ISBN 978-618-85072-0-3.
[EURODYN 2020 /11./. Athény (GR), 23.11.2020-26.11.2020]
Grant CEP: GA TA ČR(CZ) TN01000007
Institucionální podpora: RVO:61388998
Klíčová slova: stall flutter * aeroelasticity * boundary element method * discrete vortex particle method * panel method * blade cascade * Viscous-inviscid coupling
Obor OECD: Applied mechanics
Trvalý link: http://hdl.handle.net/11104/0315414