Got my EE Lightning T5 into the sim, but can only start one engine which only powers up to idle, I also have no throttle control over it so it stays at idle, anybody got ideas what to do to fix this and to get No 2 engine started ?, I also have no power to airbrakes or flaps.
Thanks
Have you checked you have two jet engines in engines.cfg?
This is what I have at the start of engines.cfg
[GENERALENGINEDATA]
; LEGACY
engine_type = 1 ; 0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine.0 = -24.00, 0.00, 1.10 ;
engine.1 = -24.00, 0.00, 3.70 ;
if that helps
Do you have other engine sections further down?
Make sure also the dependency section is copied across from the manifest.json file from a working plane too. Might already be there if you used a converter
I used the legacy importer to convert it, heres my engine.cfg file
[VERSION]
major = 1 ;
minor = 0 ;
[GENERALENGINEDATA]
; LEGACY
engine_type = 1 ; 0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine.0 = -24.00, 0.00, 1.10 ;
engine.1 = -24.00, 0.00, 3.70 ;
fuel_flow_scalar = 1.00 ; Fuel flow scalar
min_throttle_limit = -0.4 ; Minimum percent throttle. Generally negative for turbine reverser
max_contrail_temperature = -30 ;
; MODERN
;-master_ignition_switch = 0 ;
;-starter_type = 2 ; 0=Electric, 1=Manual, 2=Bleed Air
;-thrustanglespitchheading.0 = 0, 0 ;
[TURBINEENGINEDATA]
; LEGACY
fuel_flow_gain = 0.0012 ; Gain on fuel flow
inlet_area = 3.35 ; Square Feet, engine nacelle inlet area
rated_n2_rpm = 8000 ; RPM, second stage compressor rated value
static_thrust = 12690 ; Lbs, max rated static thrust at Sea Level
afterburner_available = 0 ;
afterburner_throttle_threshold = 0.65 ;
reverser_available = 1 ;
thrustspecificfuelconsumption = 1.70 ;
afterburnthrustspecificfuelconsumption = 1.90 ;
; MODERN
;-reverser_mach_controlled = 0 ;
;-mach_0_corrected_commanded_ne_table = 0.000000:1.000000:22.570000,0.000000:66.000000:82.500000,0.420000:78.800003:95.400002,0.510000:82.500000:98.500000,0.610000:87.400002:101.099998,0.700000:92.000000:103.099998,0.790000:96.199997:105.699997,0.930000:103.099998:108.059998,1.000000:105.000000:108.059998 ;
;-mach_hi_corrected_commanded_ne_table = 0.900000:1.000000:22.570000,0.000000:62.000000:82.500000,0.420000:77.000000:95.400002,0.510000:80.199997:98.500000,0.610000:84.800003:101.099998,0.700000:89.099998:103.099998,0.790000:92.199997:105.699997,0.930000:96.000000:108.059998,1.000000:98.199997:108.059998 ;
;-corrected_n2_from_ff_table = 0.000000:0.000000, 0.002940:10.000000, 0.011800:30.000000, 0.020660:40.000000, 0.033970:50.000000, 0.053170:60.000000, 0.133910:80.000000, 0.257710:90.000000, 0.540000:100.000000, 0.686860:105.000000 ;
;-n1_and_mach_on_thrust_table = 0.000000:0.000000:0.100000:0.200000:0.300000:0.400000:0.500000:0.600000:0.700000:0.800000:0.900000,0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000,20.000000:0.016000:0.017000:0.018000:0.019000:0.020000:0.021000:0.022000:0.023000:0.024000:0.025000,25.000000:0.032000:0.034000:0.036000:0.038000:0.040000:0.042000:0.044000:0.046000:0.048000:0.050000,30.000000:0.053000:0.056000:0.059000:0.062000:0.065000:0.068000:0.071000:0.074000:0.077000:0.080000,35.000000:0.084000:0.088000:0.092000:0.096000:0.100000:0.104000:0.108000:0.112000:0.116000:0.120000,40.000000:0.136000:0.142000:0.148000:0.154000:0.160000:0.166000:0.172000:0.178000:0.184000:0.190000,45.000000:0.209000:0.217000:0.225000:0.233000:0.241000:0.249000:0.257000:0.265000:0.273000:0.281000,50.000000:0.310000:0.320000:0.330000:0.340000:0.350000:0.360000:0.370000:0.380000:0.390000:0.400000,55.000000:0.423000:0.435000:0.446000:0.458000:0.470000:0.482000:0.494000:0.505000:0.517000:0.529000,60.000000:0.536000:0.551000:0.565000:0.579000:0.594000:0.608000:0.622000:0.636000:0.651000:0.665000,65.000000:0.618000:0.636000:0.653000:0.671000:0.688000:0.705000:0.723000:0.740000:0.758000:0.775000,70.000000:0.700000:0.721000:0.742000:0.763000:0.784000:0.805000:0.826000:0.847000:0.868000:0.889000,75.000000:0.772000:0.797000:0.822000:0.847000:0.872000:0.897000:0.922000:0.947000:0.972000:0.997000,80.000000:0.838000:0.868000:0.898000:0.928000:0.958000:0.988000:1.018000:1.048000:1.078000:1.108000,85.000000:0.889000:0.924000:0.959000:0.994000:1.029000:1.064000:1.099000:1.134000:1.169000:1.204000,90.000000:0.923000:0.963000:1.003000:1.043000:1.083000:1.123000:1.163000:1.203000:1.243000:1.283000,95.000000:0.964000:1.008000:1.052000:1.096000:1.140000:1.184000:1.228000:1.272000:1.316000:1.360000,100.000000:1.000000:1.038000:1.086000:1.134000:1.182000:1.230000:1.278000:1.326000:1.374000:1.422000,105.000000:1.016000:1.067000:1.118000:1.169000:1.220000:1.271000:1.322000:1.373000:1.424000:1.475000,110.000000:1.032000:1.084000:1.136000:1.188000:1.240000:1.292000:1.344000:1.396000:1.448000:1.500000 ;
;-n2_to_n1_table = 0.000000:0.000000:0.900000,0.000000:0.000000:0.000000,10.000000:2.000000:9.200000,20.000000:7.000000:14.600000,30.000000:10.200000:20.000000,40.000000:15.100000:24.700001,50.000000:20.100000:32.000000,60.000000:28.000000:41.799999,70.000000:38.000000:53.200001,80.000000:52.000000:67.500000,90.000000:70.000000:80.800003,100.000000:89.400002:100.800003,110.000000:112.000000:120.000000 ;
;-corrected_airflow_table = 0.000000:0.000000:0.100000:0.200000:0.300000:0.400000:0.500000:0.600000:0.700000:0.800000:0.900000,0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000,20.000000:2.783298:3.327631:4.346876:5.190300:5.839087:6.246526:6.700677:7.411100:8.091678:9.135577,25.000000:3.932301:4.355959:5.384287:6.293239:6.812269:7.184673:7.638175:8.288260:8.893579:9.831077,30.000000:5.067030:5.414781:6.261448:7.274854:7.743927:8.182508:8.651582:9.195914:9.770740:10.587564,35.000000:6.216682:6.473602:7.169102:8.000848:8.530258:9.105083:9.619573:10.118490:10.618056:11.358972,40.000000:7.350762:7.532423:8.061833:8.848164:9.437912:10.073075:10.602486:10.995650:11.449802:12.084965,45.000000:8.530258:8.591244:9.090161:9.725325:10.345566:11.041066:11.570477:11.903304:12.326962:12.841451,50.000000:9.650065:9.679910:10.118490:10.678393:11.283064:12.009057:12.554038:12.780465:13.173631:13.567445,55.000000:10.784146:10.784146:11.177311:11.631462:12.266625:12.962126:13.522029:13.703041:14.006024:14.262944,60.000000:11.933798:11.948720:12.372377:12.689635:13.294953:13.899624:14.610695:14.580202:14.883185:15.019431,65.000000:12.992619:13.083448:13.476614:13.793871:14.277866:14.867615:15.230935:15.458011:15.729853:15.714931,70.000000:14.172114:14.262944:14.625617:14.898108:15.291273:15.790839:16.093174:16.335173:16.561598:16.440924,75.000000:15.351610:15.472933:15.729853:16.047758:16.350094:16.743259:17.076088:17.257748:17.212332:17.121502,80.000000:16.622585:16.713415:16.955412:17.181839:17.439407:17.832573:18.074572:18.165401:18.059000:18.013586,85.000000:18.059000:18.074572:18.286076:18.452814:18.618904:18.830408:19.087976:19.042562:18.966654:18.921238,90.000000:19.632311:19.652422:19.672535:19.693296:19.713408:19.733521:19.753633:19.774395:19.794506:19.814619,95.000000:20.842299:20.862411:20.882523:20.903284:20.923397:20.943510:20.963621:20.984383:21.004496:21.024609,100.000000:21.795368:21.815479:21.835592:21.855705:21.876467:21.896578:21.916691:21.936804:21.957565:21.977676,105.000000:22.521360:22.541473:22.561586:22.581697:22.602459:22.622572:22.642685:22.662796:22.683558:22.703671,110.000000:22.898954:22.919716:22.939829:22.959942:22.980053:23.000814:23.020927:23.041040:23.061152:23.081913 ;
;-epr_max = 1.4 ;
;-epr_tc = 14 ;
;-epr_tuning_constant = 1 ;
;-oil_temp_cooling_constant = 0.21 ;
;-oil_temp_heating_constant = 700 ;
;-oil_temp_tc = 0.03 ;
;-oil_temp_tuning_constant = 1 ;
;-oil_press_max = 40003.2 ;
;-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 = 2 ;
;-egt_tuning_constant = 1 ;
;-fuel_press_max = 2376 ;
;-fuel_press_tc = 2 ;
;-fuel_press_tuning_constant = 1 ;
;-variable_inlet = 0 ;
;-primary_nozzle_available = 0 ;
;-primary_nozzle_afterburner_offset = 0.14 ;
;-primary_nozzle_n1_mach_to_nozzle_pos = 0.000000:0.000000:2.000000,53.000000:0.660000:0.100000,65.000000:0.690000:0.330000,96.000000:0.700000:0.440000 ;
;-density_on_torque_table = 0.000225:0.100000, 0.000352:0.300000, 0.000480:0.500000, 0.000607:0.700000, 0.000734:0.900000, 0.000862:1.000000, 0.001241:1.000000, 0.001620:1.000000, 0.001999:1.000000, 0.002378:1.000000 ;
;-starter_n1_max_pct = 12 ; Pct, percentage of max rpm that reached using only starter.
;-starter_n1_rate = 12 ; Rate at which the starter N1 increases.
;-ignition_auto_type = “AntiIce,Flaps” ; If the Ignition is set to AUTO - specifies how that is handled. 0(default) = Always on, 1 = Ignition follows starter status, 2 = Ignition enabled when Flaps are not neutral, when AntiIce is enabled, or when N1/N2 is below 50%.
;-min_condition_lever_for_combustion = 0.01 ; % - Minimum position of the Condition lever to obtain a combustion. Default at 0.01.
;-min_n1_for_combustion = 10 ; % - Minimum N1 required to maintain a combustion
;-min_n2_for_combustion = 19.4 ; % - Minimum N2 required to maintain a combustion
;-min_n1_for_starter_cutoff = 200 ; % - Minimum N1 at which the starter is automatically disabled
;-min_n2_for_starter_cutoff = 200 ; % - Minimum N2 at which the starter is automatically disabled
;-n1_normal_tc = 0.5 ; Float factor changing N1 acceleration during normal use of the engine
;-n1_start_max_rate = 1.0 ; Float limiting N1 acceleration during starter use
;-n1_start_combustion_max_rate = 2.0 ; Float limiting N1 acceleration during startup when cumbustion has started
;-idle_fuel_flow = 600 ; pound per hour
;-low_idle_n1 = 20 ;
;-low_idle_n2 = 60 ;
;-high_n1 = 100 ;
;-high_n2 = 100 ;
;-high_fuel_flow = 9800 ;
;-min_n2_for_fuel_flow = 22 ;
;-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 ; 0 = no protection, value of the torque triggering a protection by automatically limiting the fuelflow
;-max_n1_protection = 104 ; 0 = no protection, value of the n1 triggering a protection by automatically limiting the fuelflow
;-max_n2_protection = 105 ; 0 = no protection, value of the n2 triggering a protection by automatically limiting the fuelflow
;-max_egt_protection = 2000 ; 0 = no protection, value of the egt triggering a protection by automatically limiting the fuelflow
;-n2_from_bleed_air_psi_table = 0:0, 4:8, 10:18, 18:25 ; Table which contains the n2 generated depending on the pression from the bleed air from the APU (in psi).
;-bleed_air_on_n2_tc = 1 ; Time constant which contains the speed at which the bleed air pressure affect the N2 of the turbine.
;-n1_to_oil_pressure_table = 0:0, 0.21:0.88, 0.9:0.954, 1:1 ; % of max Oil Pressure for % N1.
[JET_ENGINE]
thrust_scalar = 1.80 ;
[PROPELLER]
thrust_scalar = 1 ; Propeller thrust scalar
propeller_diameter = 7.57 ; Propeller Diameter, (feet)
propeller_blades = 5 ; Number of propeller blades
propeller_moi = 15.85686 ; Propeller moment of inertia
propeller_type = 1 ; 0=Constant Speed, 1=Fixed Pitch
use_propeller_rpm = 0 ;
beta_max = 45 ; Maximum blade pitch angle for constant speed prop, (degrees)
beta_cruise = 45 ; usual beta in cruise (full torque) used to setup prop Cx (degrees)
beta_min = 15.6 ; Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm = 25520 ; Miminum governed RPM
prop_tc = 0.04 ; Prop time-constant
gear_reduction_ratio = 16.5 ; Propeller gear reduction ratio
fixed_pitch_beta = 0 ; Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit = 80 ; Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available = 0 ; Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available = 1 ; Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available = 1 ; Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available = 1 ; Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather = 700 ; Minimum RPM for prop feathering
beta_feather = 89 ; Feathering pitch angle (degrees)
power_absorbed_cf = 1.3 ; Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available = 0 ; Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available = 1 ; Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta = 1 ; Miminum pitch angle on ground, (degrees)
minimum_reverse_beta = -25 ; Minimum pitch angle in reverse, (degrees)
prop_reverse_max_vel = 12 ; Max uvel when reversing
prop_governor_p = 5 ; Propeller governor controller P
prop_governor_i = 3 ; Propeller governor controller I
prop_governor_d = 30 ; Propeller governor controller D
prop_governor_iboundary = 5 ; Propeller governor controller I Boundary
prop_governor_dboundary = 50 ; Propeller governor controller D Boundary
prop_cx_min = 0.06 ; Value of the propeller Cx when beta = 0
prop_cx_at_cruise_beta = 1.0 ; Value of the propeller Cx when beta = beta_max
prop_efficiency_table = 0.000000:0.000000:0.294272:0.588544:0.882816:1.134134:1.385452:1.636770:1.888088:2.003423:2.118759:2.234095:2.349430:2.466902,13.600000:0.000000:0.020000:0.100000:0.600000:0.700000:0.650000:0.500000:0.300000:0.200000:0.100000:0.000000:0.000000:0.000000,15.600000:0.085664:0.571090:0.397270:0.276355:0.202701:0.148677:0.109052:0.079987:0.069382:0.060182:0.052202:0.045281:0.039174,18.540001:0.064004:0.452578:0.640042:0.533825:0.457186:0.391550:0.335337:0.287194:0.267478:0.249115:0.232012:0.216084:0.200985,21.480000:0.053175:0.354497:0.614007:0.708994:0.639399:0.576636:0.520033:0.468987:0.447269:0.426556:0.406803:0.387964:0.369674,24.420000:0.046677:0.308364:0.566209:0.731292:0.777946:0.717831:0.662361:0.611177:0.589031:0.567687:0.547117:0.527292:0.507838,27.360001:0.042345:0.277346:0.524104:0.713060:0.812751:0.846898:0.792939:0.742417:0.720322:0.698884:0.678084:0.657904:0.637967,30.299999:0.039251:0.221985:0.430732:0.613791:0.741512:0.836936:0.895905:0.915851:0.895770:0.876129:0.856919:0.838130:0.819417,33.240002:0.032636:0.199024:0.387499:0.555438:0.675860:0.770125:0.834584:0.866743:0.870299:0.852304:0.834681:0.817423:0.800211,36.180000:0.027492:0.178508:0.348554:0.502075:0.614594:0.705839:0.772651:0.812717:0.821735:0.824748:0.808614:0.792795:0.777002,39.119999:0.023376:0.152317:0.298757:0.433669:0.535825:0.622889:0.692408:0.742423:0.758440:0.769948:0.776881:0.779197:0.765185,50.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000:0.000000 ;
prop_power_cf = 0.000000:0.000000:0.294272:0.588544:0.882816:1.134134:1.385452:1.636770:1.888088:2.003423:2.118759:2.234095:2.349430:2.466902,15.600000:0.131158:0.109298:0.087438:0.065579:0.049184:0.032789:0.016395:0.000000:-0.016395:-0.032789:-0.049184:-0.065579:-0.081973,18.540001:0.262315:0.240455:0.218596:0.196736:0.180342:0.163947:0.147552:0.131158:0.114763:0.098368:0.081973:0.065579:0.049184,21.480000:0.327894:0.306034:0.284175:0.262315:0.245920:0.229526:0.213131:0.196736:0.180342:0.163947:0.147552:0.131158:0.114763,24.420000:0.349753:0.327894:0.306034:0.284175:0.267780:0.251385:0.234991:0.218596:0.202201:0.185806:0.169412:0.153017:0.136622,27.360001:0.371613:0.349753:0.327894:0.306034:0.289639:0.273245:0.256850:0.240455:0.224061:0.207666:0.191271:0.174877:0.158482,30.299999:0.393472:0.371613:0.349753:0.327894:0.311499:0.295104:0.278710:0.262315:0.245920:0.229526:0.213131:0.196736:0.180342,33.240002:0.656656:0.634796:0.612937:0.591077:0.574682:0.558288:0.541893:0.525498:0.509104:0.492709:0.476314:0.459920:0.443525,36.180000:0.919839:0.897979:0.876120:0.854260:0.837866:0.821471:0.805076:0.788682:0.772287:0.755892:0.739497:0.723103:0.706708,39.119999:1.183022:1.161163:1.139303:1.117444:1.101049:1.084654:1.068259:1.051865:1.035470:1.019075:1.002681:0.986286:0.969891,42.060001:1.446205:1.424346:1.402486:1.380627:1.364232:1.347837:1.331443:1.315048:1.298653:1.282259:1.265864:1.249469:1.233075,45.000000:1.709389:1.687529:1.665670:1.643810:1.627415:1.611021:1.594626:1.578231:1.561837:1.545442:1.529047:1.512653:1.496258 ;
[TURBOPROP_ENGINE]
power_scalar = 1 ; Scalar on Turboprop power
maximum_torque = 2232 ; Maximum torque available (ft-lbs)
engine_friction_table = -10:-0.2, 0:0, 10:0.01, 70:0.5, 105:0.5 ; Rpm -> Friction torque
n1_to_shaft_torque_table = 0:0, 68:0.15, 92:1.0, 100:1.2, 110:1.3 ; Corrected N1 -> Shaft Torque
tp_idle_range = 12.00 ; increase of n1 idle at high mixture (Percent)
rated_shaft_hp = 0 ;
powerspecificfuelconsumption = 0.493 ; SFC
free_turbine = 1 ;
[PISTON_ENGINE]
power_scalar = 1 ; Piston power scalar
cylinder_displacement = 137.5 ; Cubic inches per cylinder
compression_ratio = 8.5 ; Compression ratio
number_of_cylinders = 4 ; Number of cylinders
max_rated_rpm = 2355 ; Max rated RPM
max_rated_hp = 300 ; Max rated HP
min_cruise_rpm = 1800 ;
max_cruise_rpm = 2355 ;
max_indicated_rpm = 2700 ;
fuel_metering_type = 0 ; 0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type = 0 ; 0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque = 0.3 ; Starter torque factor
starter_time = 1.5 ; Time the Starter stays active when pressed
turbocharged = 0 ; Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp = 29.6 ; Max design manifold pressure, (inHg)
min_design_mp = 15 ; Min design manifold pressure, (inHg)
critical_altitude = 0 ; Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type = 0 ; 0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset = 0 ; Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset = 0 ; Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture = 0 ; Automixture available? 0=FALSE, 1=TRUE
auto_ignition = 0 ; Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar = 1 ; Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar = 1 ;
max_rpm_friction_scalar = 1 ; Scalar on maximum RPM friction
idle_rpm_friction_scalar = 1 ; Scalar on idle RPM friction
bestpowerspecificfuelconsumption = 0.49 ; SFC at Best Power mixture ratio
egt_tuning_constant = 1 ;
egt_peak_temperature = 1660 ; typical peak EGT: 1200 degF + 460
egt_tc = 2 ;
cht_tuning_constant = 1 ;
cht_cooling_constant = 0.65 ;
cht_heating_constant = 960 ; max temp degrees Rankine
cht_tc = 0.015 ;
oil_press_tuning_constant = 1 ;
oil_press_max = 11520 ; max oil pressure (psf)
oil_press_tc = 0.8 ;
oil_temp_tuning_constant = 1 ;
oil_temp_cooling_constant = 0.21 ;
oil_temp_heating_constant = 700 ; max oil temperature degrees Rankine
oil_temp_tc = 0.03 ;
radiator_temp_tuning_constant = 1 ;
radiator_temp_cooling_constant = 0.015 ;
radiator_temp_max = 670 ; max radiator temperature degrees Rankine
radiator_temp_tc = 0.02 ;
fuel_press_tuning_constant = 1 ;
fuel_press_max = 2376 ; max fuel pressure (psf)
fuel_press_tc = 2 ;
number_of_magnetos = 2 ;
two_stroke_cycle = 0 ;
supercharged = 0 ;
radiator_cooling_constant = 0.015 ;
radiator_heating_constant = 670 ;
radiator_tc = 0.02 ;
radiator_tuning_constant = 1 ;
magneto_order_left_right_both = 0 ;
engine_mechanical_efficiency_table = 0:0.77, 700:0.77, 2000:0.67, 2200:0.54, 2700:0.54 ;
engine_friction_table = -300:-25, 300:25, 500:25, 2700:31 ;
manifold_efficiency_table = 0:0.2, 1:0.97 ;
rpm_to_oil_pressure_table = 0:0, 0.1:0.3, 0.2:0.9, 0.519:1, 0.74:1 ;
rpm_to_fuel_pressure_table = 0:0, 500:0.3, 1400:1, 2000:1 ;
oil_temp_factor_from_rpm = 0:0.5, 500:0.8, 2000:1.0 ;
diesel = 0 ; Is it diesel engine?
induction_air_temp_tc = 0.7 ; Induction Air Temp time constant
carb_heat_delta_temp = 55 ; Delta of temperature when the Carburator Heater is activated (In Rankine)
single_magneto_efficiency = 0.97 ; Efficiency ratio of the engine if it is designed for 2 magnetos but only 1 is currently active.
oil_temp_to_oil_pressure_table = 0:0, 500:-1, 700:-600 ; Pressure differential (in psf) of the oil depending on its temperature (in K).
shaft_torque_tc = 2 ; Gives the speed at which the shaft torque reaches its target value.
recip_stop_arc_degrees = 90 ; Gives the amplitude of the motion made by a reciprocating engine while it is having a spring compression behaviour after it stops producing work.
recip_stop_arc_restitution = 0.8 ; Gives the amount of torque in % restituted when reaching its max arc by a reciprocating engine while it is having a spring compression behaviour after it stops producing work.
recip_stop_arc_max_pct_rpm = 0.04 ; Gives the % max rpm at which a reciprocating engine that stopped producing work will start having a spring compression behaviour.
recip_stop_arc_friction_factor = 2 ; Factor on how much friction affects the reciprocating engine while having a spring compression behaviour.
egt_factor_from_pct_power = 0:0.5, 0.5:0.894, 0.64:0.956, 0.75:0.98, 1:1 ; Gives the EGT temperature factor (to egt_peak_temperature) from the pct of power (HP/maxHP)
egt_delta_from_mixture_ratio = 0.043:-100, 0.05:-89.7, 0.067:-50, 0.07:0, 0.075:-4.9, 0.083:-80, 0.108:-120.5 ; Gives the EGT temperature delta (to current egt value after factor is applied) from the mixture ratio
Thanks