Parametric Study of Ice Accretion Formation on a Swept Wing at SLD Conditions NASA Glenn Research Center

Format:

Conference/Event

Author/Creator:

Vargas, Mario, author.

Conference Name:

2007 SAE Aircraft and Engine Icing International Conference (2007-09-24 : Seville, Spain)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 2007

Summary:

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

Notes:

Vendor supplied data

Publisher Number:

2007-01-3345

Access Restriction:

Restricted for use by site license