For proof that castering wheels in the sim I have modded the dc3 to enable free castering tailwheel. THis has made taxiing far harder but more realistic as you need to use throttle, rudder and differential brakes to control the tail wheel angle, taxi-ing on a sideslope is much harder and now possible to ground loop. Definitely need tailwheel lock for takeoff
Copy this over to your flightmodel.cfg, I use it with the duckworth enhancement mod
[CONTACT_POINTS]
static_pitch = 11.5
static_cg_height = 9.5
gear_system_type = 1 ;0 = electrical, 1 = hydraulic, 2 = pneumatic, 3 = manual, 4 = none, 5 = undefined
tailwheel_lock = 1
locked_tailwheel_max_range = 0.261799
max_castering_angle = 3.14159265358979
gear_locked_on_ground = 0
gear_locked_above_speed = 250
max_speed_full_steering = 0
max_speed_decreasing_steering = 0
min_available_steering_angle_pct = 0.0
max_speed_full_steering_castering = 40
max_speed_decreasing_steering_castering = 40
min_available_steering_angle_pct = 0.0
min_castering_angle = 0.0
max_number_of_points = 15
;landing gear
point.0 = 1, -55.53, 0, -2.89, 1600, 0, 0.6, 180, 0.082, 2.5, 0.695, 0, 0, 0, 0, 0, 2 ; sta 666.4
point.1 = 1, -18.33, -9.761698, -11.25, 1600, 1, 1.875, 0, 0.704, 2.5, 0.682, 4.7, 11.5, 2, 140, 150, 2 ; sta 220
point.2 = 1, -18.33, 9.761698, -11.25, 1500, 2, 1.875, 0, 0.704, 2.5, 0.682, 5.2, 11.5, 3, 140, 150, 2 ; sta 220
;main gear retracted
;point.3 = 1, -18.33, -9.761698, -8.25, 1600, 1, 1.875, 0, 0.704, 2.5, 0.682, 0, 0, 2, 0, 0, 2 ; sta 220
;point.4 = 1, -18.33, 9.761698, -8.25, 1500, 2, 1.875, 0, 0.704, 2.5, 0.682, 0, 0, 3, 0, 0, 2 ; sta 220
;scrape points
point.3 = 2, 0, 0, 0, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0, 1 ; nose
point.4= 2, -9, 9.25, -6.757123, 800, 0, 0, 0, 0, 0, 0, 0, 0, 8, 0, 0, 1 ; right engine nacelle scrape
point.5 = 2, -9, -9.25, -6.757123, 800, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 1 ; left engine nacelle scrape
point.6 = 2, -60, -0.0, -1.637793, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0, 1 ; tail scrape
point.7 = 2, -57, -0.0, 12, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0, 1 ; top of fin
point.8 = 2, -60, -13.25, 1.5, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0, 1 ; left stab tip
point.9 = 2, -60, 13.25, 1.5, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0, 1 ; right stab tip
point.10 = 2, -26, -47, 1, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0, 1 ; left wing tip
point.11 = 2, -26, 47, 1, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0, 1 ; right wing tip
point.12 = 2, -8, 0, 4.3, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0, 1 ; fuselage top
point.13 = 2,-20.33,-9.762,-6.25,1600,0,0,0,0,0,0,0,0,0,0,0 ; left waterscrape
point.14 = 2,-20.33,9.762,-6.25,1500,0,0,0,0,0,0,0,0,0,0,0 ; right waterscrape
emergency_extension_type = 1
steering_time_constants = 3, 5
hyd_need_power_to_function = 0 ```