Meshfree reduced order model for turbomachinery blade flutter analysis

Number of the records: 1

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SYSNO	0556768
Title	Meshfree reduced order model for turbomachinery blade flutter analysis
Author(s)	Prasad, Chandra Shekhar (UT-L)_ORCID Kolman, Radek (UT-L)_RID Pešek, Luděk (UT-L)_RID
Source Title	International Journal of Mechanical Sciences. Roč. 222, May (2022). - : Elsevier
Article number	107222
Document Type	Článek v odborném periodiku
Grant	GA20-26779S GA ČR - Czech Science Foundation (CSF), CZ - Czech Republic
	EF15_003/0000493 GA MŠMT - Ministry of Education, Youth and Sports (MEYS), CZ - Czech Republic
	TN01000007 GA TA ČR - Technology Agency of the Czech Republic (TA ČR), CZ - Czech Republic
Institutional support	UT-L - RVO:61388998
Language	eng
Country	GB
Keywords	aeroelastic instability * turbomachinery blade flutter * hybrid 3D panel method * reduced order aeroelastic model * boundary element method * discrete vortex particle method
URL	https://www.sciencedirect.com/science/article/pii/S002074032200145X
Permanent Link	http://hdl.handle.net/11104/0331233

Number of the records: 1