Aircraft Thermal Management Using Loop Heat Pipes: Experimental Simulation of High Acceleration Environments Using the Centrifuge Table Test Bed
作者： Andrew J. Fleming , Quinn H. Leland , Kirk L. Yerkes , Levi J. Elston , Scott K. Thomas
DOI: 10.4271/2006-01-3066
关键词: Acceleration 、 Temperature control 、 Mechanical engineering 、 Centrifuge 、 Aerodynamic heating 、 Micro-loop heat pipe 、 Condenser (heat transfer) 、 Heat pipe 、 Loop heat pipe 、 Engineering
摘要: Abstract : The objective of this paper is to describe the design an experiment that will examine effects elevated acceleration environments on a high-temperature, titanium-water loop heat pipe for actuator cooling. An experimental test setup has been designed mounting 8-ft-diameter centrifuge table, which capable radial accelerations up 12-g's. A high-temperature PAO interface condenser simulate rejection transported temperature. In addition LHP experimentation, mathematical model developed aerodynamic heating high-speed aircraft. flat plate at zero-incidence, used aircraft wing, was subjected sub- and supersonic flow whether be rejected or absorbed. results analysis determine conditions during testing.
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