gyronewbie
New member
- Jun 2, 2003
- 1
I want to design a ducted fan. I need to evaluate air flow through the inlet, into the fan and out the exhaust. The duct is not the big problem. The big problem is modeling a rotating airfoil as the load inducer. A pressure gradient will be induced by the fan. ANSYS appears to evaluate the gradient and flow based on an input deltaP between the inlet and exhaust. So how to create a deltaP in the middle when the deltaP is a function of the combined performance of the fan and duct? Inlet Po is ambient air at V=0. P reduces due to fan suction. P increases through the fan/propeller and then decays slightly to something above ambient. I'm looking for flowstreams, velocities, and surface forces through the system.