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0524925 - ÚT 2021 RIV US eng J - Journal Article
Prasad, Chandra Shekhar - Pešek, Luděk
Efficient prediction of classical flutter stability of turbomachinery blade using the boundary element type numerical method.
Engineering Analysis With Boundary Elements. Roč. 113, April (2020), s. 328-345. ISSN 0955-7997. E-ISSN 1873-197X
R&D Projects: GA ČR GA16-04546S
Institutional support: RVO:61388998
Keywords : turbomachinery * aeroelasticity * panel method * aerodynamic damping * traveling wave mode * classical flutter * boundary element method
OECD category: Applied mechanics
Impact factor: 2.964, year: 2020
Method of publishing: Limited access
https://www.sciencedirect.com/science/article/pii/S0955799720300199?via%3Dihub
Permanent Link: http://hdl.handle.net/11104/0310312