1. K.L. Leffel, A numerical and experimental investigation of electrothermal aircraft deicing, NASA-CR-175024, NASA Lewis Research Center, 1986.
2. A heater made from graphite composite material for potential deicing application;Hung;J. Aircraft,1987
3. R.K. Jeck, Icing design envelopes (14 CFR parts 25 and 29, Appendix C) converted to a distance based format, Technical report, DOT/FAA/AR-00/30, FAA, 2002.
4. Federal Aviation Administration (FAA), Department of Transportation, Effect of icing on aircraft control and aircraft deice and anti-ice systems, AC 91-51A, 1996.
5. K. Al-Khalil, Thermo-mechanical expulsive deicing system - TMEDS, in: 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, U.S.A, 2007. https://doi.org/10.2514/6.2007-692.