Problem in solving combustion simulation
Hi friends am solving combustion problem in Fluent,.. for my geometry i have to nozzles one at inlet & other at out let,.. am getting good results inside combustion chamber but getting negative (static & absolute ) pressures at throat of the nozzles,.. what is the problem?? am unable to find where am going wrong,... can any one help me pleaseeeeeee...
|All times are GMT -4. The time now is 08:52.|