Experimental validation of FEM-computed stress to tip deflection ratios of aero-engine compressor blade vibration modes and quantification of associated uncertainties

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. 2022, 178(October), 109257. ISSN 0888-3270. E-ISSN 1096-1216. Available: doi: 10.1016/j.ymssp.2022.109257.