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SLD Instrumentation in Icing Wind Tunnels – Investigation Overview

Authors :
James T. Riley
Alexei Korolev
John W. Strapp
Judith F. Van Zante
Thomas P. Ratvasky
Biagio Esposito
David M. Orchard
Source :
AIAA AVIATION 2021 FORUM.
Publication Year :
2021
Publisher :
American Institute of Aeronautics and Astronautics, 2021.

Abstract

A collaborative effort to better understand cloud characterization probes in Supercooled Large Drop (SLD) conditions, as well the ability to simulate these conditions in several icing wind tunnels, was undertaken by NASA, NRCC, CIRA, ECCC, FAA and Met Analytics, Inc. Both drop sizing and liquid water content, LWC, were measured with various probes using current to emerging technologies. To ensure the best possible data quality from the newest probes, the probe manufacturers, SEA, Inc. and Artium, Inc. were invited to support testing and data analysis efforts. A common set of probes was identified to test in each of the three participating facilities: NRCC’s Altitude Icing Wind Tunnel, NASA’s Icing Research Tunnel and CIRA’s Icing Wind Tunnel. From the common set of probes, a subset were identified to use for comparison across the three facilities. These were the CDP-2 and 2D-S for drop sizing, and the Multi-wire for LWC. The LWC value was also checked by measuring the ice accretion thickness under hard rime conditions on a NACA-0012 airfoil. A common test matrix with sweeps in both LWC and median volume diameter, MVD, was developed. Each facility achieved these conditions as determined by their own calibration. The MVD ranged from 20 to at least 200 um, and LWC ranged from 0.5 to 3 g/m3. The comparison probes tested at common conditions in each facility were intended to allow for a direct comparison, and check of potential facility bias.

Details

Database :
OpenAIRE
Journal :
AIAA AVIATION 2021 FORUM
Accession number :
edsair.doi...........90d91128418ca6aa333315d4c4d33e4d
Full Text :
https://doi.org/10.2514/6.2021-2647