51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 2013
DOI: 10.2514/6.2013-1141
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Spray Model Evaluations for a Reverse Flow Combustor

Abstract: A previously studied computational fluid dynamic (CFD) fuel spray model used to characterize a pressure swirl atomizer under non-reacting conditions is implemented into a reverse flow combustor simulation. This spray model relies upon a stochastic secondary breakup model to predict the diameter distribution downstream of the atomizer and provides a robust method of simulating the fuel spray in CFD simulations. For 3 fuel nozzle shroud geometries, combustor simulations are performed using the aforementioned spr… Show more

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