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Experimental comparison of icing cloud instrumentsIcing cloud instruments were tested in the spray cloud Icing Research Tunnel (IRT) in order to determine their relative accuracy and their limitations over a broad range of conditions. It was found that the average of the readings from each of the liquid water content (LWC) instruments tested agreed closely with each other and with the IRT calibration; but all have a data scatter (+ or - one standard deviation) of about + or - 20 percent. The effect of this + or - 20 percent uncertainty is probably acceptable in aero-penalty and deicer experiments. Existing laser spectrometers proved to be too inaccurate for LWC measurements. The error due to water runoff was the same for all ice accretion LWC instruments. Any given laser spectrometer proved to be highly repeatable in its indications of volume median drop size (DVM), LWC and drop size distribution. However, there was a significant disagreement between different spectrometers of the same model, even after careful standard calibration and data analysis. The scatter about the mean of the DVM data from five Axial Scattering Spectrometer Probes was + or - 20 percent (+ or - one standard deviation) and the average was 20 percent higher than the old IRT calibration. The + or - 20 percent uncertainty in DVM can cause an unacceptable variation in the drag coefficient of an airfoil with ice; however, the variation in a deicer performance test may be acceptable.
Document ID
19830016216
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Olsen, W.
(NASA Lewis Research Center Cleveland, OH, United States)
Takeuchi, D. M.
(Meteorology Research, Inc.)
Adams, K.
(Air Force Flight Test Center)
Date Acquired
September 4, 2013
Publication Date
January 1, 1983
Subject Category
Air Transportation And Safety
Report/Patent Number
NAS 1.15:83340
E-1595
AIAA PAPER 83-0026
NASA-TM-83340
Report Number: NAS 1.15:83340
Report Number: E-1595
Report Number: AIAA PAPER 83-0026
Report Number: NASA-TM-83340
Meeting Information
Meeting: Aerospace Sci. Conf.
Location: Reno, NV
Country: United States
Start Date: January 10, 1983
End Date: January 13, 1983
Sponsors: AIAA
Accession Number
83N24487
Funding Number(s)
PROJECT: RTOP 505-45-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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