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Pressure Driven Supersonic Flow in Converging-Diverging Nozzle

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August 28, 2019, 01:37	CFD in Pelton turbine nozzle	#8
Bishal Pandey New Member Bishal Pandey Join Date: Aug 2019 Posts: 1 Rep Power: 0	I am having a problem keeping the total head constant. I am simulating a nozzle used in a Pelton turbine at different nozzle position. it works if I use total mass flow inlet and static pressure at the outlet. but when I move to total pressure inlet, I get "floating point error", I have tried refining the mesh also but it does not help. Have anyone has any idea about such a problem? what might be the problem?

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converging-diverging, nozzle, pressure driven, supersonic

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