Emilio, Thank you a lot for your brilliant advices!
1) Could you clarify about vehicle reference area?
I use concorde tutorial as reference for my project with surrogate aerodynamic data. in code I removed all geometry parameters, except from basic parameters (code doesn't work without vehicle.reference_area) and
instead of manually filled data for Wing, fuselage, etc. I read VSP file . Also I find out that changing: "# basic parameters vehicle.reference_area" my drag coefficients in mission are changed too, is that vehicle level reference area that you pointed out?
So what I did, I randomly picked the value vehicle.reference_area and my results from mission plots (AoA, M, Cd, CL) matched with my input data in base_data.txt. Am I did right?
2) Where is placed oswald correction? What does it?
3) I have CFD RANS data and I filled them into base_data.txt, so I wanna only interpolated my CFD data without others drag calculation in SUAVE. am I right that I should skip all drags? But to be honest when I skip one of the drags I have errors...
and why do you think that I need total drag?
Sorry for so many question. Emilio, you are my savior.
понедельник, 29 августа 2022 г. в 21:18:54 UTC+2, Emilio: