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Pneumatic boot for helicopter rotor deicingPneumatic deicer boots for helicopter rotor blades were tested. The tests were conducted in the 6 by 9 ft icing research tunnel on a stationary section of a UH-IH helicopter main rotor blade. The boots were effective in removing ice and in reducing aerodynamic drag due to ice.
Document ID
19810010533
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Blaha, B. J. (NASA Lewis Research Center Cleveland, OH, United States)
Evanich, P. L. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 11, 2013
Publication Date
March 1, 1981
Publication Information
Publication: NASA. Langley Research Center The 1980 Aircraft Safety and Operating Probl., Pt. 2
Subject Category
Air Transportation And Safety
Accession Number
81N19059
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19810010530Collected WorksThe 1980 Aircraft Safety and Operating Problems, Part 2
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