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Effects of Hydrogen Bonding and Molecular Chain Flexibility of Substituted n-Alkyldimethylsilanes On Impact Ice Adhesion Shear StrengthThe effects of hydrogen bonding and molecular flexibility upon ice adhesion shear strength were investigated using aluminum substrates coated with substituted n-alkyldimethylalkoxysilanes. The location of the chemical group substitution was on the opposing end of the linear n-alkyl chain with respect to silicon. Three hydrogen-bonding characteristics were evaluated: 1) non-hydrogen bonding, 2) donor/acceptor, and 3) acceptor. Varying the length of the n-alkyl chain provided an assessment of molecular chain flexibility. Coated and uncoated aluminum surfaces were characterized by receding water contact angle and surface roughness. Ice adhesion shear strength was determined in the Adverse Environment Rotor Test Stand facility from -16 to -8°C that simulated aircraft in-flight icing conditions within the FAR Part 25/29 Appendix C icing envelope. Surface roughness of the coatings was similar allowing for comparison of the test results. An adhesion reduction factor, based on the ice adhesion shear strength data with respect to uncoated aluminum obtained at the same temperature, was calculated to compare the data. The results revealed complex interactions with impacting supercooled water droplets that were interdependent upon ice accretion temperature, surface energy characteristics of water and ice, hydrogen bonding characteristic of the substituent, and length of the n-alkyl chain. To aid in explaining the results, 1) changes in the surface energy component (i.e., non-polar and polar) values that water undergoes during its’ phase change from liquid to solid that arise from the freezing of impacting supercooled water droplets on the surface depended upon the temperature during accretion were taken into account and 2) the physical properties (i.e., water solubility and melting point) of small compounds analogous to the substituted n-alkyldimethylalkoxysilanes used in this study were compared.

Document ID
20200002031
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Smith, Joseph G.
(NASA Langley Research Center Hampton, VA, United States)
Wohl, Christopher J.
(NASA Langley Research Center Hampton, VA, United States)
Kreeger, Richard E.
(NASA Glenn Research Center Cleveland, OH, United States)
Palacios, Jose
(Pennsylvania State Univ. University Park, PA, United States)
Hernandez, Maricely
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
March 30, 2020
Publication Date
February 1, 2020
Subject Category
Aircraft Design, Testing And Performance
Structural Mechanics
Report/Patent Number
NASA/TM-2020-220567
NF1676L-35825
L-21121
Funding Number(s)
WBS: 081876.02.07.50.08.03
Distribution Limits
Public
Copyright
Public Use Permitted.
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