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A structural dynamics investigation related to EIDI applicationsA method for modeling the structural dynamics of electro-impulse deicing is presented. A guideline for building a representative finite element model is discussed together with the experimental determination of the force pulse parameters used in the computational model. The results from the computer solution are compared with experimental results for a semi-cylindrical shell. This preliminary comparison indicated that typical structural dynamic responses may be predicted in the near coil field for the duration of the forcing pulse. The sensitivity of the response to both geometric and electrical parameters is also discussed.
Document ID
19860035204
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bernhart, W. D.
(Wichita State University KS, United States)
Gien, P. H.
(Wichita Univ. Wichita, KS, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1986
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 86-0550
Accession Number
86A19942
Funding Number(s)
CONTRACT_GRANT: NAG3-284
Distribution Limits
Public
Copyright
Other

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