Isokinetic Probe Total Water Content Measurements in the NASA Icing Research Tunnel with Supercooled Large Drop Conditions
Author:
Affiliation:
1. NASA Glenn Research Center
2. Met Analytics, Inc.
3. Science Engineering Associates
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2021-2649
Reference23 articles.
1. Wind Tunnel Measurements of the Response of Hot-Wire Liquid Water Content Instruments to Large Droplets
2. Performance of a Counterflow Virtual Impactor in the NASA Icing Research Tunnel
3. Wind Tunnel Tests of the Airborne PVM-100A Response to Large Droplets
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