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Methods for Scaling Icing Test ConditionsThis report presents the results of tests at NASA Lewis to evaluate several methods to establish suitable alternative test conditions when the test facility limits the model size or operating conditions. The first method was proposed by Olsen. It can be applied when full-size models are tested and all the desired test conditions except liquid-water content can be obtained in the facility. The other two methods discussed are: a modification of the French scaling law and the AEDC scaling method. Icing tests were made with cylinders at both reference and scaled conditions representing mixed and glaze ice in the NASA Lewis Icing Research Tunnel. Reference and scale ice shapes were compared to evaluate each method. The Olsen method was tested with liquid-water content varying from 1.3 to .8 g/m(exp3). Over this range, ice shapes produced using the Olsen method were unchanged. The modified French and AEDC methods produced scaled ice shapes which approximated the reference shapes when model size was reduced to half the reference size for the glaze-ice cases tested.
Document ID
19950012869
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Anderson, David N.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1995
Subject Category
Air Transportation And Safety
Report/Patent Number
E-9376
NASA-TM-106827
AIAA PAPER 95-0540
NAS 1.15:106827
Report Number: E-9376
Report Number: NASA-TM-106827
Report Number: AIAA PAPER 95-0540
Report Number: NAS 1.15:106827
Meeting Information
Meeting: Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 9, 1995
End Date: January 12, 1995
Accession Number
95N19284
Funding Number(s)
PROJECT: RTOP 505-68-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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