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Evaluation and Validation of the Messinger Freezing FractionOne of the most important non-dimensional parameters used in ice-accretion modeling and scaling studies is the freezing fraction defined by the heat-balance analysis of Messinger. For fifty years this parameter has been used to indicate how rapidly freezing takes place when super-cooled water strikes a solid body. The value ranges from 0 (no freezing) to 1 (water freezes immediately on impact), and the magnitude has been shown to play a major role in determining the physical appearance of the accreted ice. Because of its importance to ice shape, this parameter and the physics underlying the expressions used to calculate it have been questioned from time to time. Until now, there has been no strong evidence either validating or casting doubt on the current expressions. This paper presents experimental measurements of the leading-edge thickness of a number of ice shapes for a variety of test conditions with nominal freezing fractions from 0.3 to 1.0. From these thickness measurements, experimental freezing fractions were calculated and compared with values found from the Messinger analysis as applied by Ruff. Within the experimental uncertainty of measuring the leading-edge thickness, agreement of the experimental and analytical freezing fraction was very good. It is also shown that values of analytical freezing fraction were entirely consistent with observed ice shapes at and near rime conditions: At an analytical freezing fraction of unity, experimental ice shapes displayed the classic rime shape, while for conditions producing analytical freezing fractions slightly lower than unity, glaze features started to appear.
Document ID
20050215212
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Anderson, David N.
(Ohio Aerospace Inst. Brook Park, OH, United States)
Tsao, Jen-Ching
(Ohio Aerospace Inst. Brook Park, OH, United States)
Date Acquired
September 7, 2013
Publication Date
August 1, 2005
Subject Category
Air Transportation And Safety
Report/Patent Number
NASA/CR-2005-213852
E-15222
AIAA Paper 2003-1218
Report Number: NASA/CR-2005-213852
Report Number: E-15222
Report Number: AIAA Paper 2003-1218
Meeting Information
Meeting: 41st Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 6, 2003
End Date: January 9, 2003
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 22-728-41-17
CONTRACT_GRANT: NCC3-884
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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