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, P., Mekhalfia, M. L., Tchawou Tchuisseu, E. B. 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.