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Isokinetic Probe Total Water Content Measurements in the NASA Icing Research Tunnel with Supercooled Large Drop ConditionsAn Isokinetic Total Water Content Evaporator (IKP2) was used to measure liquid water content (LWC) in the NASA Icing Research Tunnel (IRT) with spray conditions that ranged in LWC and cloud drop size spectra as characterized by the median volumetric diameter (MVD). The IKP2 measurements were made as part of an international collaborative effort to investigate the measurement of supercooled large drop (SLD) conditions in several icing wind tunnels. This report focuses on the IKP2 and background water vapor (BWV) measurements made within the NASA IRT during the October 2017 test entry. The IKP2 TWC results are compared to the IRT LWC calibration values for a range of LWC and MVD values. The IRT LWC calibration is based on measurements from a multi-element hot-wire probe. In general, the IKP2 TWC values were approximately 9% greater than the IRT LWC calibration values over a range of LWC from 0.4 g/m3 to 3.0 g/m3. The ratio of IKP2 TWC to IRT LWC calibration ranged from approximately 0.9 to 1.27 over a range of MVD from 15um to 460 um. Comparisons of this data set to IKP2 data from a 2014 IRT test entry show similar results in the regions where overlaps occurred. The results support the theory and observations of water mass loss from hot-wire TWC sensors when subjected to large MVD conditions.
Document ID
20210021120
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Thomas P Ratvasky
(Glenn Research Center Cleveland, Ohio, United States)
J Walter Strapp
(Met Analytics, Inc)
Lyle E Lilie
(Science Engineering Associates)
Date Acquired
August 30, 2021
Publication Date
November 1, 2021
Publication Information
Subject Category
Aeronautics (General)
Report/Patent Number
E-19982
AIAA-2021-2649
NASA/TM-20210021120
Meeting Information
Meeting: AIAA Aviation 2021 Conference
Location: Virtual
Country: US
Start Date: August 2, 2021
End Date: August 6, 2021
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 951888.02.03.03.03.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
o Aircraft Icing
o Icing cloud instruments
o Aircraft instrumentation
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