Electroimpulse deicing - Electrodynamic solution by discrete elements-Reference-Cited by-同舟云学术

Electroimpulse deicing - Electrodynamic solution by discrete elements

Published:1989-06 Issue:6 Volume:26 Page:547-553
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Bernhart W. D.¹,Schrag R. L.¹

Affiliation:

1. Wichita State University, Wichita, Kansas

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.45801

Reference5 articles.

1. Production of short mechanical impulses by means of eddy currents

2. 3Henderson, R. A. "Theoretical Analysis of the Electrical Aspects of the Basic Electro-Impulse Problem in Aircraft De-Icing Applications," Ph.D. Thesis,Wichita State University, Wichita, KS, March 1986.

3. 4Bernhart, W. D. and Gien, P. H. "A Structural Dynamics Investigation Related to EIDI Applications/- AIAA Paper 86-0550, Jan. 1986.

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