I'm new to CFD, and currently trying to analyze the lift and drag forces on an rc plane that I designed in SolidWorks 2013.
The plane was designed as a single part with multiple bodies.
I followed some youtube tutorials on how to setup the parameters. I'm aware that I need to include some more specific values
in my setup, but just wanted an estimate at first.
The plane is at a zero angle of attack and being simulated at a flying speed of 75 ft/s.
The problem that I'm facing is that the output drag force value that I get is higher than the lift force value, which is incorrect.
I've attached the model and the setup that I used.
Can you guys please give me some pointers as to what I'm doing wrong and if my setup is incorrect?
Thanks in advance!