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Rotating Rig Development for Droplet Deformation/Breakup and Impact Induced by Aerodynamic SurfacesThis work presents the development of a Rotating Rig Facility by the Instituto Nacional de Tecnica Aeroespacial (INTA) in cooperation with the NASA Glenn Research Center. The facility is located at the INTA installations near Madrid, Spain. It has been designed to study the deformation, breakup and impact of large droplets induced by aerodynamic bodies. The importance of these physical phenomena is related to the effects of Supercooled Large Droplets in icing clouds on the impinging efficiency of the droplets on the body, that may change should these phenomena not be taken into account. The important variables and the similarity parameters that enter in this problem are presented. The facility's components are described and some possible set-ups are explained. Application examples from past experiments are presented in order to indicate the capabilities of the new facility.
Document ID
20120015400
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Feo, A.
(Instituto Nacional de Tecnica Aeroespacial Madrid, Spain)
Vargas, M.
(NASA Glenn Research Center Cleveland, OH, United States)
Sor, A.
(Instituto Nacional de Tecnica Aeroespacial Madrid, Spain)
Date Acquired
August 26, 2013
Publication Date
September 1, 2012
Subject Category
Air Transportation And Safety
Report/Patent Number
E-18432
SAE2011-38-0087
NASA/TM-2012-217721
Report Number: E-18432
Report Number: SAE2011-38-0087
Report Number: NASA/TM-2012-217721
Meeting Information
Meeting: SAE/AIAA International Conference on Aircraft and Engine Icing and Ground Deicing
Location: Chicago, IL
Country: United States
Start Date: June 13, 2012
End Date: June 17, 2012
Sponsors: American Inst. of Aeronautics and Astronautics, Society of Automotive Engineers, Inc.
Funding Number(s)
WBS: WBS 648987.02.03.03.10
Distribution Limits
Public
Copyright
Public Use Permitted.
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