Update latest config files
This commit is contained in:
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@ -1,4 +1,4 @@
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//TFDi Designs MD-11F (GE CF6-80C2D1F) vRC1.4_GE_F 29AUG24
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//TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.6.5_GE_F 04APR25
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[VERSION]
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//KH Bump major
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@ -1,4 +1,4 @@
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//TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.6.5_GE 04APR25
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//TFDi Designs MD-11F (P&W PW4662) vRC1.6.5_PW_F 04APR25
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[VERSION]
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major = 3
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@ -31,9 +31,9 @@ DisableAutopilotControls=1
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fuel_flow_gain=1
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low_idle_n1=24.2
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low_idle_n2=62.9
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inlet_area=9.92
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inlet_area=10.53
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rated_N2_rpm=11055
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static_thrust=61960
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static_thrust=62000
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reverser_available=1
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reverser_mach_controlled=0
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afterburner_available=0
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@ -43,24 +43,23 @@ use_commanded_Ne_Table=1
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use_corrected_N2_from_FF_table=1
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use_n2_to_n1_table=1
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use_old_fuelflow_simvar=1
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n2_to_n1_table=0:0:0.85,0:0:0,10:1.1:1,20:2.7:2.4,30:5.7:4.7,40:11.1:9.78,50:16.35:14.9,64.5:25.34:25.39,70:38:37.16,80:59.2:58.56,90:80.4:79.96,99.6:110.75:110.5,105:112:112
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mach_0_corrected_commanded_ne_table=0:1:5.42,0:64:64.5,0.143:69.214:69.857,0.286:74.428:75.214,0.429:79.642:80.571,0.572:84.856:85.928,0.715:90.07:91.285,0.858:95.284:96.642,1:100.5:102
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mach_hi_corrected_commanded_ne_table=0.88:1:5.42,0:66:67.5,0.143:71.143:72.571,0.286:76.286:77.642,0.429:81.429:82.713,0.572:86.572:87.784,0.715:91.715:92.855,0.858:96.858:97.926,1:102:103
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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
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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
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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
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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
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//KH START Modified
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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
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//KH START Modified
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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
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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
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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
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epr_max=1.8
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epr_tc=14
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epr_tuning_constant=1
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oil_temp_cooling_constant=0.21
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oil_temp_heating_constant=650
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oil_temp_heating_constant=700
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oil_temp_tc=0.07
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oil_temp_tuning_constant=1
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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
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oil_press_max=13000
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oil_press_max=38000
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oil_press_tc=0.8
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oil_press_tuning_constant=1
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itt_peak_temperature=2141
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@ -91,7 +90,7 @@ idle_fuel_flow=600
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idle_high_fuel_flow=40
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min_n2_for_fuel_flow=17
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high_n1=110
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high_n2=105
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high_n2=114
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high_fuel_flow=9800
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mach_influence_on_n1=10
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fuel_flow_max=10000
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@ -102,7 +101,7 @@ fuel_flow_controller_iboundary=10
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fuel_flow_controller_dboundary=100
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max_torque_protection=0
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max_n1_protection=110
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max_n2_protection=100
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max_n2_protection=114
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max_egt_protection=2000
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fuel_flow_max_itt_factor=2
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fuel_flow_min_itt_factor=0.9
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@ -1,4 +1,4 @@
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//TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.4_GE 29AUG24
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//TFDi Designs MD-11F (P&W PW4662) vRC1.6.5_PW_F 04APR25
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[VERSION]
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//KH Bump major
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@ -7,7 +7,7 @@ minor = 1
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[WEIGHT_AND_BALANCE]
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max_gross_weight = 630500
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empty_weight = 283975
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empty_weight = 248567
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reference_datum_position = 0, 0, 0
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empty_weight_CG_position = -13.3, 0, 0
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CG_forward_limit = 0.13
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@ -18,28 +18,22 @@ empty_weight_yaw_MOI = 40761191
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empty_weight_coupled_MOI = 0
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activate_mach_limit_based_on_cg = 0
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activate_cg_limit_based_on_mach = 0
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max_number_of_stations = 21
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max_number_of_stations = 15
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station_load.0=170.0, 82.0, -2.0, 4.0, Pilot, 1
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station_load.1=170.0, 82.0, 2.0, 4.0, First Officer, 2
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station_load.2=170.0, 80.0, 3.3, 4.0, Engineer, 0
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station_load.3=850.0, 66.0, 0.0, 4.0, Cabin crew 1, 0
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station_load.4=680.0, 45.0, -5.0, 4.0, Business 1 L, 0
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station_load.5=680.0, 45.0, 0.0, 4.0, Business 1 C, 0
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station_load.6=680.0, 45.0, 5.0, 4.0, Business 1 R, 0
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station_load.7=680.0, 25.0, -5.0, 4.0, Business 2 L, 0
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station_load.8=960.0, 25.0, 0.0, 4.0, Business 2, 0
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station_load.9=680.0, 25.0, 5.0, 4.0, Business 2 R, 0
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station_load.10=5723.0, -20.0, -5.0, 4.0, Economy 3 L, 0
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station_load.11=5724.0, -20.0, 0.0, 4.0, Economy 3 C, 0
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station_load.12=5723.0, -20.0, 5.0, 4.0, Economy 3 R, 0
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station_load.13=9066.0, -50.0, -5.0, 4.0, Economy 4 L, 0
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station_load.14=9067.0, -50.0, 0.0, 4.0, Economy 4 C, 0
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station_load.15=9066.0, -50.0, 5.0, 4.0, Economy 4 R, 0
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station_load.16=850.0, -55.0, 0.0, 4.0, Cabin crew 2, 0
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station_load.17=28648.0, 20.0, 0.0, -4.5, Forward cargo, 0
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station_load.18=38648.0, -50.0, 0.0, -4.5, Rear cargo, 0
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station_load.19=0.0, 5.0, -2.0, -4.5, Left aux tank, 0
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station_load.20=0.0, 5.0, 2.0, -4.5, Right aux tank, 0
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station_load.3=8675.0, 60.0, -5.0, 4.0, Upper zone 1 L, 0
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station_load.4=8675.0, 60.0, 5.0, 4.0, Upper zone 1 R, 0
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station_load.5=11675.0, 10.0, -5.0, 4.0, Upper zone 2 L, 0
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station_load.6=11675.0, 10.0, 5.0, 4.0, Upper zone 2 R, 0
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station_load.7=11675.0, -40.0, -5.0, 4.0, Upper zone 3 L, 0
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station_load.8=11675.0, -40.0, 5.0, 4.0, Upper zone 3 R, 0
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station_load.9=14675.0, -90.0, -5.0, 4.0, Upper zone 4 L, 0
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station_load.10=14675.0, -90.0, 5.0, 4.0, Upper zone 4 R, 0
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station_load.11=44648.0, 30.0, 0.0, -4.5, Lower forward cargo, 0
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station_load.12=64685.0, -50.0, 0.0, -4.5, Lower rear cargo, 0
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station_load.13=0.0, 5.0, -2.0, -4.5, Left aux tank, 0
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station_load.14=0.0, 5.0, 2.0, -4.5, Right aux tank, 0
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[CONTACT_POINTS]
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static_pitch = 0
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@ -126,7 +120,7 @@ vtail_sweep = 43
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vtail_pos_lon = -79.5
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vtail_pos_vert = 28
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vtail_thickness_ratio = 0.03
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fuselage_length = 202.16
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fuselage_length = 200.92
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fuselage_diameter = 19.75
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fuselage_center_pos = 10, 0, 1.0
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elevator_area = 327.0
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@ -161,7 +155,7 @@ fly_by_wire = 0
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elevator_elasticity_table = 0:0.7, 87:0.3, 210:0.5, 315:0.5
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aileron_elasticity_table = 0:1, 300:0.7, 600:0.6, 1500:0.4
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rudder_elasticity_table = 0:1, 300:1, 800:1, 1000:0.7
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elevator_trim_elasticity_table = 0:0.0, 87:0.40, 240:0.73, 290:0.73, 315:0.65
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elevator_trim_elasticity_table = 0:0.0, 87:0.40, 240:0.44, 290:0.44, 315:0.40
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[AERODYNAMICS]
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lift_coef_pitch_rate = -8.09375
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@ -323,10 +317,9 @@ best_glide = 0
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max_gear_extended = 200
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[INTERACTIVE POINTS]
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number_of_interactive_points = 3
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interactive_point.0 = 0.4, 44.15, -10.05, -0.567, 0, 0, 0, -88, 35, 0, 35, 0, 2, 33
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interactive_point.1 = 0.4, 75.65, 7.92, -0.567, 0, 0, 0, 75, 33, 2, 33, 2, 2, 33
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interactive_point.2 = 0.4, 33.3, 6.28, -7.18, 1, 0, 0, 90, 0, 0, 0, 0, 0, 0
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number_of_interactive_points = 2
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interactive_point.0 = 0.4, 75.65, -8.12, -0.567, 0, 0, 0, -75, 33, 2, 33, 2, 2, 33
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interactive_point.1 = 0.4, 33.3, 6.28, -7.18, 1, 0, 0, 90, 0, 0, 0, 0, 0, 0
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[STALL PROTECTION]
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stall_protection = 1 ; Alpha Protection
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@ -359,7 +352,6 @@ flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
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flaps-position.6 = 35, 160, 0.32, 1
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flaps-position.7 = 50, 150, 0.33, 1
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[FLAPS.1]
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type = 1
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system_type = 1
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@ -369,7 +361,7 @@ damaging-speed = 250
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blowout-speed = 300
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maneuvering_flaps = 0
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lift_scalar = 0.1
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drag_scalar = 1.1 ;1.5
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drag_scalar = 1.1
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pitch_scalar = 1
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max_on_ground_position = 7
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flaps-position.0 = 0, -1, 0
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@ -381,7 +373,6 @@ flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
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flaps-position.6 = 35, 160, 0.32, 1
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flaps-position.7 = 50, 150, 0.33, 1
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[FLAPS.2]
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type = 2
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system_type = 1
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@ -2,7 +2,7 @@
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"cells": [
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{
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"cell_type": "code",
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"execution_count": 9,
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"execution_count": 63,
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"id": "21e0ac82",
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"metadata": {},
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"outputs": [],
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@ -14,7 +14,7 @@
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},
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{
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"cell_type": "code",
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"execution_count": 10,
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"execution_count": 64,
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"id": "653d2200",
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"metadata": {},
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"outputs": [],
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@ -30,7 +30,7 @@
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},
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{
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"cell_type": "code",
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"execution_count": null,
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"execution_count": 65,
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"id": "ecfc5eed",
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"metadata": {},
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"outputs": [],
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@ -48,7 +48,7 @@
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},
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{
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"cell_type": "code",
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"execution_count": 12,
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"execution_count": 66,
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"id": "ddbebf95",
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"metadata": {},
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"outputs": [],
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@ -59,7 +59,7 @@
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},
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{
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"cell_type": "code",
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"execution_count": 30,
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"execution_count": 67,
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"id": "c65ab937",
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"metadata": {},
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"outputs": [
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@ -204,7 +204,7 @@
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},
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{
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"cell_type": "code",
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"execution_count": 62,
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"execution_count": 68,
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"id": "c2d4f3af",
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"metadata": {},
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"outputs": [
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@ -258,12 +258,6 @@
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"\n",
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"print(output)"
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]
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},
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{
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"cell_type": "markdown",
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"id": "5ac65794",
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"metadata": {},
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"source": []
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}
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],
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"metadata": {
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