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Batailly, A., Agrapart, Q., Millecamps, A., & Brunel, J.-F. (2016). Experimental and numerical simulation of a rotor/stator interaction event localized on a single blade within an industrial high-pressure compressor. Journal of Sound and Vibration, 375, 308-331. Lien externe
Batailly, A., Legrand, M., Millecamps, A., & Garcin, F. (2015). Conjectural bifurcation analysis of the contact-induced vibratory response of an aircraft engine blade. Journal of Sound and Vibration, 348, 239-262. Lien externe
Batailly, A., Legrand, M., Millecamps, A., Cochon, S., & Garcin, F. (2015). Redesign of a high-pressure compressor blade accounting for nonlinear structural interactions. Journal of Engineering for Gas Turbines and Power, 137(2), 8 pages. Lien externe
Batailly, A., Legrand, M., Millecamps, A., & Garcin, F. (juin 2014). High-pressure compressor blade dynamics under aerodynamic and unilateral contact forcings [Communication écrite]. ASME Turbo Expo 2014: Turbine Technical Conference and Exposition, Düsseldorf, Germany (8 pages). Lien externe
Batailly, A., Legrand, M., Millecamps, A., & Garcin, F. (juin 2012). Numerical study of a rotor/stator interaction case experimentally simulated with an industrial compressor [Communication écrite]. ASME Turbo Expo 2012: Turbine Technical Conference and Exposition, Copenhagen, Denmark. Lien externe
Batailly, A., Legrand, M., Millecamps, A., & Garcin, F. (2012). Numerical-experimental comparison in the simulation of rotor/stator interaction through blade-tip/abradable coating contact. Journal of Engineering for Gas Turbines and Power, 134(8), 11 pages. Lien externe
Khalifeh, E., Piollet, E., Millecamps, A., & Batailly, A. (juin 2017). Non-Linear Modeling Of Centrifugal Stiffening Effects For Accurate Bladed Component Reduced-Order Models [Communication écrite]. ASME Turbo Expo: Turbine Technical Conference and Exposition (ASME Turbo Expo 2017), Charlotte, NC (10 pages). Lien externe
Millecamps, A., Batailly, A., Legrand, M., & Garcin, F. (juin 2015). Snecma's viewpoint on the numerical and experimental simulation of blade-tip/casing unilateral contacts [Communication écrite]. ASME Turbo Expo 2015: Turbine Technical Conference and Exposition, Montréal, Québec (11 pages). Lien externe
