I did some work on it, awhile ago, but had to stop to work on other things. While being far from finished, the following changes can be made to improve the takeoff situation. Going from top to bottom,
In order to closely match the chart,
empty_weight_CG_position = -0.3, 0, 0
CG_forward_limit = 0.16
CG_aft_limit = 0.29
station_load.0 = 200, 11.2, 0, 0.8, Pilot, 1
Change fuel tank positions
Center1 = 6.31,0,0.79,230,0
Center2 = -1.5, 0, -1.3,560,6
Correct Geometry
wing_area = 260
wing_span = 27.5
wing_dihedral = 2.41
wing_virtualdihedral = 0
wing_incidence = 0
oswald_efficiency_factor = 0.85
htail_area = 35.21
htail_incidence = 0
elevator_area = 11.33
rudder_area = 9.21
elevator_up_limit = 25
elevator_down_limit = 15
aileron_up_limit = 20
aileron_down_limit = 20
rudder_limit = 24
Replace the elevator trim limit with the following
;elevator_trim_limit = 20 ; Elevator trim max angle (absolute value) (DEGREES)
elevator_trim_up_limit = 12.25
elevator_trim_down_limit = 1
elevator_trim_neutral = 8
Based on glide performance, the drag coefficient can be determined
The best glide for range occurs at Cl = 0.4, with ratio 9.9
In the aerodynamics section,
drag_coef_zero_lift = 0.0202
Set the lift slope for a symmetrical airfoil at 0 incidence, appropriate for the aspect ratio and sweep
lift_coef_aoa_table = -0.39:-0.88, 0.39:0.88
In the flight tuning section,
elevator_trim_effectiveness = 1.3
That's as far as I've gotten. Can't say when I'll be able to finish it, but hopefully soonish...
Testing the Lift/Drag ratio in the sim, it's pretty close at 10.1, vs the calculated 9.9
Any performance discrepencies after this are due to engine/thrust and not drag.