Hi, I have ran a simulation with my plane model and all the coeficents seems to be incorrect except for the lift coefficient. I know for sure the drag coefficient isn’t 0.18 and the moment coefficient isn’t more than 0.01. I dont know why this is happening can you please help me.
Thank you so much for your time and effort,
Hi Frank, thank you for using the forum
There could be many reasons why the results are not expected, but in order to acknowledge them, I will need to check your setup. Is it possible that you send the link please?
Also, what are your expectations regarding the results?
Hi Frank, I hope you are well, apologies for the delay!
I have two basic questions;
- Why do you need a moving wall for your aircraft simulation?
- Do you have a reference paper you are comparing your results with? Feel free to add it so I can check it
Hey, any updates on this?