NASA NTRS · 19840037099
Electro-impulse deicing - Structural dynamic studies, icing tunnel tests and applications
Abstract
This paper contains a discussion of the comparison of analytical and experimental results of the dynamic response of a flat rectangular plate subjected to electro-impulse type deicing forces. Early attempts in this correlation have been hampered by the complex leading edge geometries of the airfoils tested to date. The lack of a suitable analytical model for a typical leading edge structure has prompted these preliminary investigations of simple geometries, beginning with a flat plate and to be followed by a semi-cylindrical leading edge representation. The comparisons reported herein are thus limited to rectangular plate models. Project plans and icing tunnel results are given.
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Bernhart, W. D., Zumwalt, G. W.. 1984-01-01. Electro-impulse deicing - Structural dynamic studies, icing tunnel tests and applications. https://ntrs.nasa.gov/citations/19840037099
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