NASA NTRS · 20130000320
Development of 3D Ice Accretion Measurement Method
Abstract
Icing wind tunnels are designed to simulate in-flight icing environments. The chief product of such facilities is the ice accretion that forms on various test articles. Documentation of the resulting ice accretion key piece of data in icing-wind-tunnel tests. Number of currently used options for documenting ice accretion in icing-wind-tunnel testing.
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Lee, Sam, Broeren, Andy P., Addy, Harold E., Jr., Sills, Robert, Pifer, Ellen M.. 2012-06-25. Development of 3D Ice Accretion Measurement Method. https://ntrs.nasa.gov/citations/20130000320
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