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0556768 - ÚT 2023 RIV GB eng J - Journal Article
Prasad, Chandra Shekhar - Kolman, Radek - Pešek, Luděk
Meshfree reduced order model for turbomachinery blade flutter analysis.
International Journal of Mechanical Sciences. Roč. 222, May (2022), č. článku 107222. ISSN 0020-7403. E-ISSN 1879-2162
R&D Projects: GA ČR(CZ) GA20-26779S; GA MŠMT(CZ) EF15_003/0000493; GA TA ČR(CZ) TN01000007
Institutional support: RVO:61388998
Keywords : aeroelastic instability * turbomachinery blade flutter * hybrid 3D panel method * reduced order aeroelastic model * boundary element method * discrete vortex particle method
OECD category: Applied mechanics
Impact factor: 7.3, year: 2022
Method of publishing: Limited access
https://www.sciencedirect.com/science/article/pii/S002074032200145X
Permanent Link: http://hdl.handle.net/11104/0331233