Comparability of Hot-Wire Estimates of Liquid Water Content in SLD Conditions 2023-01-1423
Future compliance to FAA 14 CFR Part 25 and EASA CS-25 Appendix O conditions has required icing wind tunnels to expand their cloud simulation envelope, and demonstrate accurate calibration of liquid water content and droplet particle size distributions under these conditions. This has led to a renewed community interest in the accuracy of these calibrations, and the potential inter-facility bias due to the choice of instrumentation and processing methods. This article provides a comparison of the response of various hot-wire liquid water content instruments under Appendix C and supercooled large droplet conditions, after an independent similar analysis at other wind tunnel facilities. The instruments are being used, or are under consideration for use, by facilities collaborating in the ICE GENESIS program. For droplet median volume diameters (MVDs) between about 15 and 250 μm, cylindrical hot wire LWC sensors were found to consistently and increasingly under-read measurements from conical and trough TWC sensors as MVD increased, and were not considered further. Of the remaining TWC sensors, the specific instruments investigated were found to agree within about ± 20% of their average test point response for the range of conditions tested, but systematic scale differences between instruments were found to reach about a factor of 1.4. Sensitivity to increasing droplet MVD was concluded to be similar amongst different instruments given the uncertainties, except for two that exhibited notable roll-off with MVD relative to the others.
Citation: Esposito, B., Orchard, D., Lucke, J., Nichman, L. et al., "Comparability of Hot-Wire Estimates of Liquid Water Content in SLD Conditions," SAE Int. J. Adv. & Curr. Prac. in Mobility 6(3):1119-1139, 2024, https://doi.org/10.4271/2023-01-1423. Download Citation
Author(s):
Biagio M. Esposito, David Orchard, Johannes Lucke, Leonid Nichman, Natalia Bliankinshtein, Lyle Lilie, Pietro Catalano, Francesco D'Aniello, J. Walter Strapp
Affiliated:
CIRA Scpa, National Research Council Canada, Deutsches Zentrum fur Luft und Raumfahrt, Science Engineering Associates Inc, Met Analytics Inc.
Pages: 21
Event:
International Conference on Icing of Aircraft, Engines, and Structures
e-ISSN:
2641-9645
Also in:
SAE International Journal of Advances and Current Practices in Mobility-V133-99EJ
Related Topics:
Wind tunnel tests
Three-way catalysts
Sensors and actuators
Simulation and modeling
Calibration
Measurements
Logistics
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