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An Investigation Utilizing an Electrical Analogue of Cyclic Deicing of Hollow Steel Propellers with Internal Electric HeatersA study has been made of the heating requirements for the cyclic de?icing of hollow steel propellers fitted with two types of internal electric heaters. Solutions to the transient?teat?flow equations depicting the cyclic de?icing of propellers were obtained by use of an electrical analogy. The study showed the impracticability of using an internal tubular heater and illustrated the advantages of employing an internal shoe?type heater, which distributes the heat more evenly to the blade surface. The importance of minimizing the thermal inertia of the system was demonstrated, and the magnitude of reductions in the total energy requirement made possible through reductions in the heating period was indicated.
Document ID
19810068624
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Technical Note
Authors
Neel, Carr B., Jr.
(National Advisory Committee for Aeronautics. Ames Aeronautical Lab. Moffett Field, CA, United States)
Date Acquired
August 11, 2013
Publication Date
October 1, 1953
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NACA-TN-3025
Report Number: NACA-TN-3025
Accession Number
81N73046
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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