Subsonic stall flutter analysis in 2D blade cascade using hybrid boundary element method

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SYSNO	0535111
Title	Subsonic stall flutter analysis in 2D blade cascade using hybrid boundary element method
Author(s)	Prasad, Chandra Shekhar (UT-L)_ORCID Pešek, Luděk (UT-L)_{RID, ORCID}
Source Title	EURODYN 2020, Proceedings of the XI International Conference on Structural Dynamics, 1. S. 213-224. - Athens : National Technical University of Athens (NTUA), 2020 / Papadrakakis M. ; Fragiadakis M. ; Papadimitriou C.
Conference	EURODYN 2020 /11./, 23.11.2020 - 26.11.2020, Athény
Document Type	Konferenční příspěvek (zahraniční konf.)
Grant	TN01000007 GA TA ČR - Technology Agency of the Czech Republic (TA ČR), CZ - Czech Republic
Institutional support	UT-L - RVO:61388998
Language	eng
Country	GR
Keywords	stall flutter * aeroelasticity * boundary element method * discrete vortex particle method * panel method * blade cascade * Viscous-inviscid coupling
Permanent Link	http://hdl.handle.net/11104/0315414

Number of the records: 1