|August 28, 2007, 00:41||
Hi, I'm trying to simulate a propeller using fan bc. what I confuse is about the post processing.
if i input the pressure drop (delta p) and the velocity (V) at the inlet, what will be the output?
if the output is thrust (T), aren't we able to count T = delta p x A (disk area) directly. I think i missed something here.
Thank you in advance.
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