Optimal allocation of thermodynamic irreversibility for the integrated design of propulsion and thermal management systems
More electric aircraft systems, high power avionics, and a reduction in heat sink capacity have placed a larger emphasis on correctly satisfying aircraft thermal management requirements during conceptual design. Thermal management systems must be capable of dealing with these rising heat loads, whil...
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Georgia Institute of Technology
2013
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| Online Access: | http://hdl.handle.net/1853/45913 |