Rotating Rig Development for Droplet Deformation/Breakup and Impact Induced by Aerodynamic Surfaces

2011-38-0087

06/13/2011

Event
SAE 2011 International Conference on Aircraft and Engine Icing and Ground Deicing
Authors Abstract
Content
This work presents the development of a Rotating Rig Facility by the Instituto Nacional de Técnica 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 setups are explained. Application examples from past experiments are presented in order to indicate the capabilities of the new facility.
Meta TagsDetails
DOI
https://doi.org/10.4271/2011-38-0087
Pages
30
Citation
Feo, A., Vargas, M., and Sor, S., "Rotating Rig Development for Droplet Deformation/Breakup and Impact Induced by Aerodynamic Surfaces," SAE Technical Paper 2011-38-0087, 2011, https://doi.org/10.4271/2011-38-0087.
Additional Details
Publisher
Published
Jun 13, 2011
Product Code
2011-38-0087
Content Type
Technical Paper
Language
English