TY - GEN
T1 - Experimental measurement of ice accretion due to mixed-phase icing clouds
AU - Yan, Sihong
AU - Palacios, Jose
N1 - Publisher Copyright:
© 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
Copyright:
Copyright 2018 Elsevier B.V., All rights reserved.
PY - 2018
Y1 - 2018
N2 - The ingestion of ice crystals can result in engine icing incidents. These ice crystals are ingested into the engine, become partially melted and freeze on low pressure stators and casing. This paper introduces a series of mixed-icing experiments conducted inside the Pennsylvania State University Icing Wind Tunnel (PSU-IWT). The objective was to investigate how surface temperature and percentage melting of the icing cloud affect the ice accretion rate. An icing cloud was sprayed into the wind tunnel providing fully frozen water droplets. The fully glaciated cloud was partially melted using hot air ingestion. A NACA 0012 airfoil, instrumented with two thermocouples, was used as the test article. The temperature at the leading edge was maintained using internal temperature controlled airflow. The experimental results shows how variations from fully frozen to fully partially melted clouds affect the ice accretion thickness. Within the range of test conditions discussed in the paper, the ice accretion decreases with increases of the temperature of the ingested air. The increment of surface temperature reduces ice accretion until the surface temperature reached-10 °C. The erosion effect in PSU-IWT is less significant compared with results from similar test facilities. The capability of PSU-IWT in mixed-phase icing is verified and preliminary test results are shown.
AB - The ingestion of ice crystals can result in engine icing incidents. These ice crystals are ingested into the engine, become partially melted and freeze on low pressure stators and casing. This paper introduces a series of mixed-icing experiments conducted inside the Pennsylvania State University Icing Wind Tunnel (PSU-IWT). The objective was to investigate how surface temperature and percentage melting of the icing cloud affect the ice accretion rate. An icing cloud was sprayed into the wind tunnel providing fully frozen water droplets. The fully glaciated cloud was partially melted using hot air ingestion. A NACA 0012 airfoil, instrumented with two thermocouples, was used as the test article. The temperature at the leading edge was maintained using internal temperature controlled airflow. The experimental results shows how variations from fully frozen to fully partially melted clouds affect the ice accretion thickness. Within the range of test conditions discussed in the paper, the ice accretion decreases with increases of the temperature of the ingested air. The increment of surface temperature reduces ice accretion until the surface temperature reached-10 °C. The erosion effect in PSU-IWT is less significant compared with results from similar test facilities. The capability of PSU-IWT in mixed-phase icing is verified and preliminary test results are shown.
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U2 - 10.2514/6.2018-4222
DO - 10.2514/6.2018-4222
M3 - Conference contribution
AN - SCOPUS:85051631233
SN - 9781624105586
T3 - 2018 Atmospheric and Space Environments Conference
BT - 2018 Atmospheric and Space Environments Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 10th AIAA Atmospheric and Space Environments Conference, 2018
Y2 - 25 June 2018 through 29 June 2018
ER -