NASA NTRS · 19860035202
Designing an electro-impulse de-icing system
Abstract
Basic principles and parameters for a system to deice aircraft with electromagnetic impulses are described. The physical basis for deicing by such impulses is explained, and the requirements involved in the electrodynamic design, structural dynamic design, and system design are discussed. Some manufacturing and testing problems and techniques are described.
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Zumwalt, G. W., Friedberg, R. A.. 1986-01-01. Designing an electro-impulse de-icing system. https://ntrs.nasa.gov/citations/19860035202
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