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modeling of a pulsejet in flight

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August 30, 2005, 18:31	modeling of a pulsejet in flight	#1
Tony Guest Posts: n/a	We want to model a pulsejet engine in flight. To make this simple suppose the jet is flying at a constant speed of 30m/s. The pulsejet has an inlet facing to the flight direction. Air enters the pulsejet through the inlet and react with fuel in the combustion chamber. I am not sure what kind of boundary conditions should be specified at the pulsejet inlet and the outlet. For the static case, we specified 'total pressure'at the inlet and the outlet. Thanks.

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