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Parametric Study of Ice Accretion Formation on a Swept Wing at SLD Conditions
Technical Paper
2007-01-3345
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
An experiment was conducted in the Icing Research Tunnel (IRT) at NASA Glenn Research Center to study the effect of sweep angle and temperature on the formation of ice accretions on a NACA 0012 swept wing at SLD conditions. From a baseline Appendix-C condition with a MVD of 20m the drop size was changed to 110 and 200m for the SLD cases. Casting data, ice shape tracings, time-sequence and photographic data were obtained. Time-sequence photography was taken during each run to capture in real time the formation of the ice accretion. Measurements of the critical distance were obtained.
Citation
Vargas, M. and Tsao, J., "Parametric Study of Ice Accretion Formation on a Swept Wing at SLD Conditions," SAE Technical Paper 2007-01-3345, 2007, https://doi.org/10.4271/2007-01-3345.Also In
References
- Vargas, M. “Ice Accretion on Swept Wings at Glaze Ice Conditions” Case Western Reserve University Cleveland, Ohio May 1998
- Vargas, M. Reshotko, E. “Physical Mechanisms of Glaze Ice Scallop Formations on Swept Wings” AIAA Paper 98-0491 Jan. 1998
- Vargas, M. Reshotko, E. “LWC and Temperature Effects on Ice Accretion Formation on Swept Wings at Glaze Ice Conditions” AIAA Paper 2000-00483 Jan. 2000
- Vargas, M. Reshotko, E. “Parametric Experimental Study of the Formation of Glaze Ice Shapes on Swept Wings” AIAA Paper 99-0094 Jan. 1999