Parametric Study of Ice Accretion Formation on a Swept Wing at SLD Conditions
Document Number: 2007-01-3345
Date Published: September 2007
Author(s):
Mario Vargas - NASA Glenn Research Center
Jen-Ching Tsao - Ohio Aerospace Institute
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 20 \gmm the drop size was changed to 110 and 200 \gmm 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 other papers presented at 2007 SAE Aircraft and Engine Icing International Conference, September 2007, Seville, SPAIN, Session: SLD Engineering Tools Development
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