Number of the records: 1
Experimental validation of FEM-computed stress to tip deflection ratios of aero-engine compressor blade vibration modes and quantification of associated uncertainties
- 1.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
OECD category: Applied mechanics
Impact factor: 8.4, year: 2022
Method of publishing: Open access
https://www.sciencedirect.com/science/article/pii/S0888327022004058/pdfft?isDTMRedir=true&download=true
https://hdl.handle.net/11104/0335685
Number of the records: 1