K. McCarthy, E. A. Walters, A. Heltzel, PC Krause and Associates, Inc; R. Elangovan, G. Roe, W. Vannice, Boeing; C. Schemm, Lockheed Martin; J. Dalton, Avetec; S. Iden, P. Lamm, C. Miller, U.S. Air Force Research Laboratory; A. Susainathan, U.S. Air Force Aeronautical Systems Center
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 nonproprietary 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.
2008 SAE Power Systems Conference, November 11-13 2008, Bellevue, WA. Paper #2008-01-2899