Ice Accretions on a Swept GLC-305 Airfoil NASA Glenn Research Center

Format:

Conference/Event

Author/Creator:

Vargas, Mario, author.

Conference Name:

General Aviation Technology Conference & Exhibition (2002-04-16 : Wichita, Kansas, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 2002

Summary:

An experiment was conducted in the Icing Research Tunnel (IRT) at NASA Glenn Research Center to obtain castings of ice accretions formed on a 28° swept GLC-305 airfoil that is representative of a modern business aircraft wing. Because of the complexity of the casting process, the airfoil was designed with three removable leading edges covering the whole span. Ice accretions were obtained at six icing conditions. After the ice was accreted, the leading edges were detached from the airfoil and moved to a cold room. Molds of the ice accretions were obtained, and from them, urethane castings were fabricated. This experiment is the icing test of a two-part experiment to study the aerodynamic effects of ice accretions

Notes:

Vendor supplied data

Publisher Number:

2002-01-1519

Access Restriction:

Restricted for use by site license