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Acceptable Tolerances for Matching Icing Similarity Parameters in Scaling ApplicationsThis paper reviews past work and presents new data to evaluate how changes in similarity parameters affect ice shapes and how closely scale values of the parameters should match reference values. Experimental ice shapes presented are from tests by various researchers in the NASA Glenn Icing Research Tunnel. The parameters reviewed are the modified inertia parameter (which determines the stagnation collection efficiency), accumulation parameter, freezing fraction, Reynolds number, and Weber number. It was demonstrated that a good match of scale and reference ice shapes could sometimes be achieved even when values of the modified inertia parameter did not match precisely. Consequently, there can be some flexibility in setting scale droplet size, which is the test condition determined from the modified inertia parameter. A recommended guideline is that the modified inertia parameter be chosen so that the scale stagnation collection efficiency is within 10 percent of the reference value. The scale accumulation parameter and freezing fraction should also be within 10 percent of their reference values. The Weber number based on droplet size and water properties appears to be a more important scaling parameter than one based on model size and air properties. Scale values of both the Reynolds and Weber numbers need to be in the range of 60 to 160 percent of the corresponding reference values. The effects of variations in other similarity parameters have yet to be established.
Document ID
20030064040
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Anderson, David N.
(Ohio Aerospace Inst. Brook Park, OH, United States)
Date Acquired
September 7, 2013
Publication Date
June 1, 2003
Subject Category
Aerodynamics
Report/Patent Number
E-13514
NASA/CR-2003-211822
AIAA Paper 2001-0832
NAS 1.26:211822
Report Number: E-13514
Report Number: NASA/CR-2003-211822
Report Number: AIAA Paper 2001-0832
Report Number: NAS 1.26:211822
Meeting Information
Meeting: 39th Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 8, 2001
End Date: January 11, 2001
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NCC3-884
WORK_UNIT: WU-708-20-13-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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