Application of Electrohydrodynamic (EHD) Heat Transfer Enhancement to Aircraft Environmental Control Systems

1999-01-2164

07/12/1999

Event
International Conference On Environmental Systems
Authors Abstract
Content
Electrohydrodynamic (EHD) heat transfer enhancement is a technology that may yield substantial reductions in heat exchanger weight and volume, as well as “on-demand” heat transfer. An overall assessment of the applicability of EHD to aircraft systems is given and key areas for future investigation to enable application are identified. A brief review of the underlying physics and key factors for the application of EHD to an aircraft Environmental Control System (ECS) is given. The major engineering challenges involved in application of EHD to an aircraft system are discussed. Potential system impacts of an EHD-enhanced ECS heat exchanger are explored.
Meta TagsDetails
DOI
https://doi.org/10.4271/1999-01-2164
Pages
9
Citation
Paschkewitz, J., "Application of Electrohydrodynamic (EHD) Heat Transfer Enhancement to Aircraft Environmental Control Systems," SAE Technical Paper 1999-01-2164, 1999, https://doi.org/10.4271/1999-01-2164.
Additional Details
Publisher
Published
Jul 12, 1999
Product Code
1999-01-2164
Content Type
Technical Paper
Language
English