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Dynamic Thermal Management System Modeling of a More Electric Aircraft P.C. Krause and Associates, Incorporated

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
McCarthy, K., author.
Conference Name:
Power Systems Conference (2008-11-11 : Seattle, Washington, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 2008
Summary:
Advancements in electrical, mechanical, and structural design onboard modern more electric aircraft have added significant stress to the thermal management systems (TMS). A thermal management system level analysis tool has been created in MATLAB/Simulink to facilitate rapid system analysis and optimization to meet the growing demands of modern aircraft. It is anticipated that the tracking of thermal energy through numerical integration will lead to more accurate predictions of worst case TMS sizing conditions. In addition, the non-proprietary nature of the tool affords users the ability to modify component models and integrate advanced conceptual designs that can be evaluated over multiple missions to determine the impact at a system level
Notes:
Vendor supplied data
Publisher Number:
2008-01-2886
Access Restriction:
Restricted for use by site license

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