The Effect of Stainless Steel 304 Surface Roughness on Ice Adhesion Shear Strength of Accreted Impact IceAircraft in-flight icing is problematic due to the ad-verse effect on vehicle performance. It occurs when supercooled water droplets (SCWD) present in clouds, under the appropriate environmental conditions, col-lide with the aircraft surface resulting in accretion of ice (i.e., impact icing). Impact ice can range from clear/glaze to rime or a combination of the two (i.e., mixed) with the type determined by the air temperature (0 to -20°C), liquid water content (LWC, 0.3-0.6 g/cu.m), and droplet size [median volumetric diameter (MVD) of 15-40 µm] present during accretion.1 These impact icing events generally occur at temperatures ranging from 0 to -20°C. Below -20°C, ice crystals dominate the environment and typically do not adhere to the aircraft surface. A main difference between an impact icing occurrence and a slow growth icing (i.e., freezer ice) one is the speed of the icing event. Besides environmental conditions, ice adhesion strength (IAS) to a metallic substrate depends upon surface roughness. It is known that increasing surface roughness and decreasing temperature lead to in-creases in IAS.
Document ID
20200002450
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Smith, Joseph G., Jr. (NASA Langley Research Center Hampton, VA, United States)
Wohl, Christopher J. (NASA Langley Research Center Hampton, VA, United States)
Culver, Gabriel F. (New Horizons Governor's School for Science and Technology Hampton, VA, United States)
Denkins, Max H. (NASA Langley Research Center Hampton, VA, United States)
Chauby, Michael J. (NASA Langley Research Center Hampton, VA, United States)
Beck, Devon M. (NASA Langley Research Center Hampton, VA, United States)