Finite element studies of the electro impulse de-icing system

Author:

Scavuzzo R. J.1,Chu M. L.1,Woods E. J.2,Raju R.1,Khatkhate A. A.3

Affiliation:

1. University of Akron, Akron, Ohio 44325

2. Boeing Commercial Airplane Company, Seattle, Washington

3. Innovative Dynamics, Ithaca, New York

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference5 articles.

1. Electro-impulse deicing - Concept and electrodynamic studies

2. A finite element study of the EIDI system

3. 5Smythe, W. R., Static and Dynamic Electricity, McGraw-Hill, New York, 1950, pp.290, 291.

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2. Modelling electro-impulse de-icing process in leading edge structure and impact fatigue life prediction of rivet holes in critical areas;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2019-12-21

3. On measuring key parameters of an electro-impulse deicing system;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2018-04-29

4. Simulation and validation of slat de-icing by an electromechanical system;CEAS Aeronautical Journal;2014-11-25

5. Coupled Magnetic and Structural Numerical Simulation and Experimental Validation of the Electro Impulse De-Icing;54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2013-04-05

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