@MaverickF22:
Hello again,
Thanks for telling me about these aspects…, so as i’ve also noticed, there is a great difference in drag between OFM and AFM and now i have my answer in that multiplier (only for CD). About the lift (CL) values…, i can’t obtain some better ones at the moment, but i’ll keep trying to get them to more correct areas, while the drag values, as far as i know, are a bit higher than they should, though i hope they respect a realistic form as they travel from -90 to +90 AoA and from Mach = 0 to 2.5. About the thrust tables, Mav also gave me a more clear view and as it seems i confused the static thrust with the one at a higher Mach number, so i’ll try to correct that as well.
Have a good day!
So it will be easier.
Add a few charts from practical aerodynamics of the MiG-23ML.
23_Cl_local_AOA
X-axis = Cl.
Y-axis = local_AOA (units); localAOA= 2 * trueAOA – 5.5
23_Cl_to_M
X-axis = Cl
Y-axis = Mach number.
23_Cdo
X-axis = Cd0 with different sweep of wing.
Y-axis = Mach number.
23_Cl_to_Cd
X-axis = Cl
Y-axis = Cd (total)
The top chart for wing sweep = 45 with two R-23
The bottom chart for a clean aircraftwith different swept wing.
23_AC
for Mach number = 0.6
X-axis = aerodynamic quality (Cl/Cd)
Y-axis = Cl
23_trust
X-axis = Thrust with lossy in the inlet and nozzle (installed trust)
Y-axis = Mach number.
the dotted line – Thrust Full AB
dashed line with a point - military power