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Additional Study of Water Droplet Median Volume Diameter (MVD) Effects on Ice ShapesThis paper reports the result of an experimental study in the NASA Glenn Icing Research Tunnel (IRT) to evaluate how well the MVD-independent effect identified previously might apply to SLD conditions in rime icing situations. Models were NACA 0012 wing sections with chords of 53.3 and 91.4 cm. Tests were conducted with a nominal airspeed of 77 m/s (150 kt) and a number of MVD's ranging from 15 to 100 m with LWC of 0.5 to 1 g/cu m. In the present study, ice shapes recorded from past studies and recent results at SLD and Appendix-C conditions are reviewed to show that droplet diameter is not important to rime ice shape for MVD of 30 microns or larger, but for less than 30 m drop sizes a rime ice shape transition from convex to wedge to spearhead type ice shape is observed.
Document ID
20050215215
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Tsao, Jen-Ching
(Ohio Aerospace Inst. Brook Park, OH, United States)
Anderson, David N.
(Ohio Aerospace Inst. Brook Park, OH, United States)
Date Acquired
September 7, 2013
Publication Date
August 1, 2005
Subject Category
Air Transportation And Safety
Report/Patent Number
E-15223
NASA/CR-2005-213853
AIAA Paper 2004-0413
Report Number: E-15223
Report Number: NASA/CR-2005-213853
Report Number: AIAA Paper 2004-0413
Meeting Information
Meeting: 42nd Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 5, 2004
End Date: January 8, 2004
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NCC3-938
WBS: WBS 22-728-41-17
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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