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A Procedure for the Design of Air-Heated Ice-Prevention SystemsA procedure proposed for use in the design of air-heated systems for the continuous prevention of ice formation on airplane components is set forth. Required heat-transfer and air-pressure-loss equations are presented, and methods of selecting appropriate meteorological conditions for flight over specified geographical areas and for the calculation of water-drop-impingement characteristics are suggested. In order to facilitate the design, a simple electrical analogue was devised which solves the complex heat-transfer relationships existing in the thermal-system analysis. The analogue is described and an illustration of its application to design is given.
Document ID
19810068602
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Technical Note
Authors
Neel, C. B.
(National Advisory Committee for Aeronautics. Ames Aeronautical Lab. Moffett Field, CA, United States)
Date Acquired
August 11, 2013
Publication Date
June 1, 1954
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NACA-TN-3130
Report Number: NACA-TN-3130
Accession Number
81N73024
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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