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Conjectural bifurcation analysis of an aircraft engine blade undergoing 3D unilateral contact constraints

Alain Batailly and Mathias Legrand

Paper (2014)

Document published while its authors were not affiliated with Polytechnique Montréal

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PolyPublie URL: https://publications.polymtl.ca/12773/
Conference Title: ASME Turbo Expo 2014: Turbine Technical Conference and Exposition
Conference Location: Düsseldorf, Germany
Conference Date(s): 2014-06-16 - 2014-06-20
Publisher: American Society of Mechanical Engineers (ASME)
DOI: 10.1115/gt2014-25674
Official URL: https://doi.org/10.1115/gt2014-25674
Date Deposited: 18 Apr 2023 15:07
Last Modified: 05 Apr 2024 10:52
Cite in APA 7: Batailly, A., & Legrand, M. (2014, June). Conjectural bifurcation analysis of an aircraft engine blade undergoing 3D unilateral contact constraints [Paper]. ASME Turbo Expo 2014: Turbine Technical Conference and Exposition, Düsseldorf, Germany (10 pages). https://doi.org/10.1115/gt2014-25674

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