Košík

0563591 - ÚT 2023 RIV GB eng J - Článek v odborném periodiku
Mohamed, E.M. - Bonello, P. - Russhard, P. - Procházka, Pavel - Mekhalfia, Mohammed Lamine - Tchawou Tchuisseu, Eder Batista
Experimental validation of FEM-computed stress to tip deflection ratios of aero-engine compressor blade vibration modes and quantification of associated uncertainties.
Mechanical Systems and Signal Processing. Roč. 178, October (2022), č. článku 109257. ISSN 0888-3270. E-ISSN 1096-1216
Grant CEP: GA MŠMT(CZ) EF15_003/0000493
Grant ostatní: AV ČR(CZ) StrategieAV21/3
Program: StrategieAV
Institucionální podpora: RVO:61388998
Klíčová slova: blade tip timing * FEM validation * vibration measurements * blade stresses
Obor OECD: Applied mechanics
Impakt faktor: 8.4, rok: 2022
Způsob publikování: Open access
https://www.sciencedirect.com/science/article/pii/S0888327022004058/pdfft?isDTMRedir=true&download=true
Trvalý link: https://hdl.handle.net/11104/0335685