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- W3034268051 abstract "We describe the steady state and transient thermal response of the aft cabin of an aircraft that is retrofitted with high-power electronic equipment and cooled by heat rejection through the skin. In this skin-cooling design, the outer surface of the fuselage is treated as a heat exchanger. Hot air from an equipment exhaust plenum is drawn into a series of baffled ducts within the fuselage support structure, where heat is rejected and then recirculated into the cabin. The cooler air from the cabin is then drawn into the electronic equipment. The aircraft air-conditioning unit is also modeled to provide chilled air directly Into the cabin. In addition, this paper presents an algorithm and a control-system concept to maintain the temperature of the aft cabin within acceptable limits. Results establish a control-system design, which is being implemented in a CL-600 Challenger aircraft" @default.
- W3034268051 created "2020-06-19" @default.
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- W3034268051 date "1998-01-12" @default.
- W3034268051 modified "2023-09-27" @default.
- W3034268051 title "Performance prediction and control system design of an aircraft skin cooling technique" @default.
- W3034268051 cites W2011260759 @default.
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- W3034268051 doi "https://doi.org/10.2514/6.1998-837" @default.
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