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.
Parametric Study of Ice Accretion Formation on a Swept Wing at SLD Conditions
Sae Technical Papers
2007 SAE Aircraft and Engine Icing International Conference ; 2007
2007-09-24
Aufsatz (Konferenz)
Englisch
Parametric Study of Ice Accretion Formation on a Swept Wing at SLD Conditions
British Library Conference Proceedings | 2007
|Swept wing ice accretion modeling
AIAA | 1990
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