TECHNICAL PAPERS

Parametric Study of Ice Accretion Formation on a Swept Wing at SLD Conditions

Date Published: 2007-09-24
Paper Number: 2007-01-3345
DOI: 10.4271/2007-01-3345

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, doi:10.4271/2007-01-3345.

Author(s):

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.

File Size: 850K

Product Status: In Stock

See papers presented at 2007 SAE Aircraft and Engine Icing International Conference, September 2007, Seville, SPAIN, Session: SLD Engineering Tools Development

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