TFDi_MD-11_QA/xkhofmann-tfdidesign-md11-config-tweaks
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Update to latest configs

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Add pax
This commit is contained in:
Kilian Hofmann
2025-06-02 20:32:45 +02:00
parent 3a2fbbbd3f
commit b499b82d8b
5 changed files with 859 additions and 146 deletions
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PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_PW/engines.cfg
-115
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@@ -1,115 +0,0 @@
//TFDi Designs MD-11F (P&W PW4662) vRC1.6.5_PW_F 04APR25
[VERSION]
//KH Bump major
major = 4
minor = 1
[GENERALENGINEDATA]
engine_type =1
fuel_flow_scalar =0.031
min_throttle_limit =-0.25
master_ignition_switch =0
starter_type =0
max_contrail_temperature =-25
Engine.0 = -3.00, -27.75, -8.50
ThrustAnglesPitchHeading.0 = 0, 0
Engine.1 = -103.50, 0.00, 15.00
ThrustAnglesPitchHeading.1 = 0, 0
Engine.2 = -3.00, 27.75, -8.50
ThrustAnglesPitchHeading.2 = 0, 0
accumulated_time_hobbs_min_pct_rpm=0
accumulated_time_hobbs_min_knots=0
[DISABLED_CONTROLS]
DisableFuelValveControls =0
DisableMixtureControls =1
DisableParkingBrakeControls =0
DisablePropellerControls =1
DisableAutopilotControls=1
[TURBINEENGINEDATA]
fuel_flow_gain=1
low_idle_n1=24.2
low_idle_n2=62.9
inlet_area=10.53
rated_N2_rpm=11055
static_thrust=62000
reverser_available=1
reverser_mach_controlled=0
afterburner_available=0
afterburner_throttle_threshold=0
ThrustSpecificFuelConsumption=0.362
use_commanded_Ne_Table=1
use_corrected_N2_from_FF_table=1
use_n2_to_n1_table=1
use_old_fuelflow_simvar=1
n2_to_n1_table=0:0:0.85,0:0:0,10:1.1:1,20:2.7:2.4,30:5.7:4.7,40:11.1:9.78,50:16.35:14.9,64.54:31.14:30.59,70.28:36.78:35.84,80.12:58.56:57.84,90.37:88.27:87.84,102.67:107.24:106.84,112:120:120
mach_0_corrected_commanded_ne_table=0:1:5.42,0:63.0:63.5,0.17:69.3:70.2,0.34:76.2:76.8,0.51:83:83.5,0.67:89.8:90.2,0.83:96.7:96.9,0.99:103.5:103.5,1:116.6:117
mach_hi_corrected_commanded_ne_table=0.88:1:5.42,0:66:66.5,0.25:77.1:79.2,0.33:81.4:83.8,0.5:88.4:90.7,0.66:94.3:97.0,0.85:96.2:99.7,0.9:101.2:105.4,1:116.2:121.2
corrected_n2_from_ff_table=0:17,0.0099:63.7,0.02:70.5,0.03:73.1,0.04:79.4,0.05:83.6,0.06:89.5,0.07:94.8,0.08:100.1,0.09:106.5
n1_and_mach_on_thrust_table=0.000000:0.000000:0.206803:0.280661:0.354519:0.428377:0.502235:0.576093:0.649951:0.723810:0.797668,0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000,20.000000:0.020334:0.018926:0.018365:0.017768:0.017149:0.016515:0.015863:0.015208:0.014534:0.013860,25.000000:0.029434:0.027422:0.026632:0.025797:0.024940:0.024059:0.023152:0.022235:0.021306:0.020375,30.000000:0.033986:0.030672:0.028919:0.026653:0.025928:0.025184:0.025802:0.021374:0.018702:0.023291,35.000000:0.070581:0.064962:0.062424:0.059648:0.056670:0.053536:0.050308:0.046924:0.043444:0.039910,40.000000:0.115706:0.107129:0.103436:0.099453:0.095210:0.090734:0.086072:0.081361:0.076653:0.071841,45.000000:0.164968:0.152931:0.147828:0.142341:0.136513:0.130440:0.124498:0.118283:0.111870:0.105388,50.000000:0.218546:0.202746:0.196107:0.188982:0.181423:0.174048:0.166338:0.158287:0.149967:0.142050,55.000000:0.276676:0.256828:0.248552:0.239686:0.230419:0.221263:0.211681:0.201686:0.191443:0.181712,60.000000:0.339274:0.315126:0.305110:0.294428:0.283152:0.272084:0.260539:0.248522:0.236179:0.224430,65.000000:0.406072:0.377362:0.365531:0.352959:0.339697:0.326347:0.312745:0.298645:0.284078:0.270104,70.000000:0.476658:0.443151:0.429436:0.414899:0.399618:0.383785:0.368032:0.351772:0.335030:0.318542,75.000000:0.550568:0.512033:0.496350:0.479778:0.462414:0.444307:0.426075:0.407561:0.388596:0.369500,80.000000:0.627228:0.583453:0.565725:0.547049:0.527537:0.507273:0.486477:0.465611:0.444349:0.422704,85.000000:0.705886:0.656705:0.636874:0.616041:0.594344:0.571897:0.548783:0.525433:0.501810:0.477902,90.000000:0.785094:0.730712:0.708789:0.685821:0.661969:0.637381:0.612132:0.586376:0.560384:0.534209,95.000000:0.863065:0.803680:0.779839:0.754920:0.729110:0.702557:0.675366:0.647478:0.619241:0.590907,100.000000:0.936071:0.872277:0.847042:0.820755:0.793551:0.765559:0.736891:0.707114:0.677066:0.646923,105.000000:0.994083:0.928996:0.903986:0.877967:0.850934:0.822172:0.792494:0.762245:0.731543:0.700495,110.000000:0.974676:0.921881:0.905331:0.888737:0.871094:0.851457:0.828909:0.802711:0.772336:0.737555
corrected_airflow_table=0:0:0.9,0:0:0,20:4.29:14.08,85:4.62:24,90:5.75:25,95:7.23:27,100:8.36:28,105:9.29:29,120:10.94:30
n2_and_mach_to_epr_table=0:0:0.242:0.413:0.452:0.613:0.673:0.763:0.82:0.84,0:0:0:0:0:0:0:0:0:0,66:0.568:0.570:0.600:0.800:1.100:1.250:1.850:2.000:2.300,89:0.610:0.612:0.820:1.038:1.210:1.350:2.150:2.177:2.700,93:0.625:0.638:0.850:1.048:1.073:1.301:2.040:2.532:2.600,97:0.940:0.959:0.950:1.055:0.913:1.526:2.785:2.991:4.050,100:1.600:1.500:1.900:2.500:3.000:3.500:3.900:4.300:5.230
JET_density_on_FF_table=0.000462:28.74,0.000587:32.93,0.000738:35.02,0.000891:29.46,0.001066:31.02,0.001267:32.56,0.001496:34.54,0.0017565:35.11,0.002048:30.8,0.002377:22.55
epr_max=1.8
epr_tc=14
epr_tuning_constant=1
oil_temp_cooling_constant=0.21
oil_temp_heating_constant=700
oil_temp_tc=0.07
oil_temp_tuning_constant=1
oil_temp_factor_from_rpm=0.00:0.80, 250.00:0.80, 500.00:0.80, 2500.00:1.00, 4000.00:1.00
oil_press_max=38000
oil_press_tc=0.8
oil_press_tuning_constant=1
itt_peak_temperature=2141
itt_tc=2
itt_tuning_constant=1
egt_peak_temperature=1600
egt_tc=0.1
egt_tuning_constant=0.1
fuel_press_max=2376
fuel_press_tc=2
fuel_press_tuning_constant=1
variable_inlet=0
primary_nozzle_available=0
starter_N1_max_pct=40
starter_N1_rate=200
starter_time=45
ignition_auto_type=""
min_condition_lever_for_combustion=0.01
min_n1_for_combustion=2
min_n2_for_combustion=17
min_n1_for_starter_cutoff=7
min_n2_for_starter_cutoff=45
min_n2_for_apu_bleed_air_cutoff=50
n1_normal_tc=0.5
n1_start_max_rate=1
n1_start_combustion_max_rate=2
idle_fuel_flow=600
idle_high_fuel_flow=40
min_n2_for_fuel_flow=17
high_n1=110
high_n2=114
high_fuel_flow=9800
mach_influence_on_n1=10
fuel_flow_max=10000
fuel_flow_controller_p=0.5
fuel_flow_controller_i=0.01
fuel_flow_controller_d=0.1
fuel_flow_controller_iboundary=10
fuel_flow_controller_dboundary=100
max_torque_protection=0
max_n1_protection=110
max_n2_protection=114
max_egt_protection=2000
fuel_flow_max_itt_factor=2
fuel_flow_min_itt_factor=0.9
n1_cooling_factor=0.01
n2_from_bleed_air_psi_table=0.0:0.0, 4.0:8.0, 10.0:18.0, 18.0:25.0
bleed_air_on_n2_tc=1
N1_to_oil_pressure_table=0.00:0.00, 0.21:0.71, 0.90:0.99, 1.00:1.00
[JET_ENGINE]
thrust_scalar=1.0
PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_PW/flight_model.cfg
+17 -17
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@@ -1,4 +1,4 @@
//TFDi Designs MD-11F (P&W PW4662) vRC1.6.5_PW_F 04APR25
//TFDi Designs MD-11F (P&W PW4660) vRC1.7.0_PW_F 15MAY25
[VERSION]
//KH Bump major
@@ -10,7 +10,7 @@ max_gross_weight = 630500
empty_weight = 248567
reference_datum_position = 0, 0, 0
empty_weight_CG_position = -13.3, 0, 0
CG_forward_limit = 0.13
CG_forward_limit = 0.12
CG_aft_limit = 0.34
empty_weight_pitch_MOI = 20897456
empty_weight_roll_MOI = 6368555
@@ -22,16 +22,16 @@ max_number_of_stations = 15
station_load.0=170.0, 82.0, -2.0, 4.0, Pilot, 1
station_load.1=170.0, 82.0, 2.0, 4.0, First Officer, 2
station_load.2=170.0, 80.0, 3.3, 4.0, Engineer, 0
station_load.3=8675.0, 60.0, -5.0, 4.0, Upper zone 1 L, 0
station_load.4=8675.0, 60.0, 5.0, 4.0, Upper zone 1 R, 0
station_load.5=11675.0, 10.0, -5.0, 4.0, Upper zone 2 L, 0
station_load.6=11675.0, 10.0, 5.0, 4.0, Upper zone 2 R, 0
station_load.7=11675.0, -40.0, -5.0, 4.0, Upper zone 3 L, 0
station_load.8=11675.0, -40.0, 5.0, 4.0, Upper zone 3 R, 0
station_load.9=14675.0, -90.0, -5.0, 4.0, Upper zone 4 L, 0
station_load.10=14675.0, -90.0, 5.0, 4.0, Upper zone 4 R, 0
station_load.11=44648.0, 30.0, 0.0, -4.5, Lower forward cargo, 0
station_load.12=64685.0, -50.0, 0.0, -4.5, Lower rear cargo, 0
station_load.3=8675.0, 55.0, -5.0, 4.0, Upper zone 1 L, 0
station_load.4=8675.0, 55.0, 5.0, 4.0, Upper zone 1 R, 0
station_load.5=11675.0, 20.0, -5.0, 4.0, Upper zone 2 L, 0
station_load.6=11675.0, 20.0, 5.0, 4.0, Upper zone 2 R, 0
station_load.7=11675.0, -20.0, -5.0, 4.0, Upper zone 3 L, 0
station_load.8=11675.0, -20.0, 5.0, 4.0, Upper zone 3 R, 0
station_load.9=14675.0, -50.0, -5.0, 4.0, Upper zone 4 L, 0
station_load.10=14675.0, -50.0, 5.0, 4.0, Upper zone 4 R, 0
station_load.11=64648.0, 30.0, 0.0, -4.5, Lower forward cargo, 0
station_load.12=44685.0, -30.0, 0.0, -4.5, Lower rear cargo, 0
station_load.13=0.0, 5.0, -2.0, -4.5, Left aux tank, 0
station_load.14=0.0, 5.0, 2.0, -4.5, Right aux tank, 0
@@ -111,7 +111,7 @@ htail_area = 920
htail_span = 59.5
htail_pos_lon = -88
htail_pos_vert = 5.0
htail_incidence = 1.0
htail_incidence = 0.8
htail_sweep = 36.5
htail_thickness_ratio = 0.02
vtail_area = 760
@@ -155,7 +155,7 @@ fly_by_wire = 0
elevator_elasticity_table = 0:0.7, 87:0.3, 210:0.5, 315:0.5
aileron_elasticity_table = 0:1, 300:0.7, 600:0.6, 1500:0.4
rudder_elasticity_table = 0:1, 300:1, 800:1, 1000:0.7
elevator_trim_elasticity_table = 0:0.0, 87:0.40, 240:0.44, 290:0.44, 315:0.40
elevator_trim_elasticity_table = 0:0.0, 87:0.40, 240:0.60, 295:1.00, 315:1.00
[AERODYNAMICS]
lift_coef_pitch_rate = -8.09375
@@ -383,7 +383,7 @@ blowout-speed = 300
maneuvering_flaps = 0
lift_scalar = 0.5
// KH From 0.75
drag_scalar = 0.75
drag_scalar = 0.475
pitch_scalar = 1
max_on_ground_position = 1
flaps-position.0 = 0, -1, 0
@@ -399,8 +399,8 @@ blowout-speed = 300
maneuvering_flaps = 0
lift_scalar = 0.5
// KH From 0.75
drag_scalar = 0.75
drag_scalar = 0.475
pitch_scalar = 1
max_on_ground_position = 1
flaps-position.0 = 0, -1, 0
flaps-position.1 = 20, 215, 0.5, 0.5
flaps-position.1 = 20, 215, 0.5, 0.5