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

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Paschkewitz, John S., author.
Conference Name:
International Conference On Environmental Systems (1999-07-12 : Denver, Colorado, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1999
Summary:
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
Notes:
Vendor supplied data
Publisher Number:
1999-01-2164
Access Restriction:
Restricted for use by site license

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