BMS4 AoA test with F-15, possible upgrade, player's aspect

[molnibalage83]

I did not touch any FM curve. I used the old FM, I just set lower to max. AoA limit, because of obvious reasons. It is clearly seen what is the useful range. Drag and lift coefficient are the following at M0.6 on 20,25,30,35 and 40 deg of AoA.

CL

0.7500 0.8200 0.8500 0.8500 0.8000

CD

0.2818 0.4100 0.5382 0.6664 0.7945

On 30 deg. the lift coeff is about 15% bigger, drag is 91% (!) bigger.

[RobertoGardi]

??? Are you working on a F-15 advanced flight model, or is this a test with the old flight model?