Parameters for Aircraft EHD Heat Exchanger Development

981292

04/21/1998

Event
Aerospace Power Systems Conference
Authors Abstract
Content
Electrohydrodynamic (EHD) forces acting on a fluid can be used to significantly increase the heat transfer coefficient with little power consumption or flow restriction. Experiments have shown promising results with simple configurations, but practical heat exchanger development is needed. Analytical development will establish design equations and aid in experimental data correlation. Small scale test units will provide experience in determining heat exchanger configurations and electrode options. Controller and high voltage power supply units will also need to be developed. Full-scale EHD heat exchanger systems can then be developed to demonstrate technology availability for military and commercial products.
Meta TagsDetails
DOI
https://doi.org/10.4271/981292
Pages
7
Citation
Haskin, W., and Paschkewitz, J., "Parameters for Aircraft EHD Heat Exchanger Development," SAE Technical Paper 981292, 1998, https://doi.org/10.4271/981292.
Additional Details
Publisher
Published
Apr 21, 1998
Product Code
981292
Content Type
Technical Paper
Language
English