Design Of Supersonic Nozzles For Ultra-Rapid Quenching Of Metallic Vapours

CSIRO has been experimenting with supersonic flows as a method of rapidly quenching metallic vapours. Cooling rates above 106 °C/s have been achieved. The supersonic flow conditions are achieved by adiabatic expansion of the vapour through a Laval nozzle into a vacuum chamber. This paper will describe the basic physics of the process, outlining computer fluid dynamic (CFD) modelling of flow in the nozzle, the effects of different flow conditions on the condensation process and discuss the practical design issues associated with operating supersonic nozzles. Results obtained from a CFD model of the nozzle, which compared two methods of incorporating condensation, showed that inclusion of condensation substantially changes the conditions in the nozzle. Most noticeably, the effect of condensation produces a region in the nozzle where the temperature remains almost constant.