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In the context of this page, the word cloud was generated from the publications of the author {}. The words in this cloud come from the titles, abstracts, and keywords of the author's articles and research papers. By analyzing this word cloud, you can get an overview of the most recurring and significant topics and research areas in the author's work.
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Khalifeh, E., Piollet, E., Millecamps, A., & Batailly, A. (2017, June). Non-Linear Modeling Of Centrifugal Stiffening Effects For Accurate Bladed Component Reduced-Order Models [Paper]. ASME Turbo Expo: Turbine Technical Conference and Exposition (ASME Turbo Expo 2017), Charlotte, NC (10 pages). External link
Batailly, A., Agrapart, Q., & Millecamps, A. (2016, June). Experimental and numerical simulation of a contact induced rotor/stator interaction inside an aircraft engine high-pressure compressor [Paper]. ASME Turbo Expo: Turbine Technical Conference and Exposition (GT2016), Seoul, South Korea (10 pages). External link
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. External link
Batailly, A., & Millecamps, A. (2016, June). Minimising clearance consumption: a key factor for the design of blades robust to rotor/stator interactions ? [Paper]. ASME Turbo Expo: Turbine Technical Conference and Exposition (GT2016), Seoul, South Korea (8 pages). External link
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. External link
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. External link
Millecamps, A., Batailly, A., Legrand, M., & Garcin, F. (2015, June). Snecma's viewpoint on the numerical and experimental simulation of blade-tip/casing unilateral contacts [Paper]. ASME Turbo Expo 2015: Turbine Technical Conference and Exposition, Montréal, Québec (11 pages). External link
Batailly, A., Legrand, M., Millecamps, A., & Garcin, F. (2014, June). High-pressure compressor blade dynamics under aerodynamic and unilateral contact forcings [Paper]. ASME Turbo Expo 2014: Turbine Technical Conference and Exposition, Düsseldorf, Germany (8 pages). External link
Batailly, A., Legrand, M., Millecamps, A., & Garcin, F. (2012, June). Numerical study of a rotor/stator interaction case experimentally simulated with an industrial compressor [Paper]. ASME Turbo Expo 2012: Turbine Technical Conference and Exposition, Copenhagen, Denmark. External link
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. External link