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J18Dread

FM modeling: Is there a how to?

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I have been trying to create mmp (online) FMs for the D7F, Spad 13, N28, and the Pfalz D12 with disappointing results, especially after the Expansion Pack.

 

My goal is parity. I want mmp to be about the pilot, not the plane. So within strict limits, I want the planes to have the same speed, the same rate of climb (+/- 10%), and turning radius (+/- 10%). This means that some planes will climb a little faster or turn a little sharper but run at about the same speed.

 

Try as I might for 'normalization', I cannot do it. I can achieve what I think are the correct settings against AI in Coop and then be disappointed when flying in Dogfight. Any suggestions? Is there an FM Guide for Dummies? My search results have not been fruitful. Thanks

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I don't know about the +/- 10% factor, but if you want all the planes to perform the same just copy the FM data from the aircraft you want and paste it in each aircraft data.ini. If you keep the first section (MissionData) for each A/C you should be OK.

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Maybe you have already seen this Notes...last update end of 2006...

 

http://www.users.bigpond.net.au/CharlesEAW/sfpage.html

 

http://www.users.bigpond.net.au/charleseaw/zips/SFNotes.zip

 

New notes specially for EP1.... do not know if there are any...

 

EmlD

 

Thanks EmID the zip file was about what I was looking for, at least it tells me what the factors mean.

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I don't know about the +/- 10% factor, but if you want all the planes to perform the same just copy the FM data from the aircraft you want and paste it in each aircraft data.ini. If you keep the first section (MissionData) for each A/C you should be OK.

 

Eventually we will get coop to work. At which point we will want to fly teams - allies vs. huns.

 

As you will notice, we have models from Third Wire and from other sources. They seem to need their individual data.inis, but I could be wrong. I have not tried to exchange the data.inis. because I still want the planes to have some 'personality', within a narrow range. Kind of like the match of a Mig15 vs. F86 - equal but different.

 

Thanks for your suggestions. I may try the exchange and see how it works.

Edited by J18Dread

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J18Dread, if you wont several planes to have equal speed... change give them the same motor, set same speed... check the EmptyInertia(x,y,z), mass etc.

 

Be careful with other sections, sections declaring the behavior of plane parts (like [TopWingLeft] or [VertTail] etc. there are more then 10 in data ini), there are references ti the nodes (meshes) like RemoveNode[001]=Tail Wire L or RemoveNode[002]=Tail Wire R or just like ModelNodeName=Tail

They refer to LOD mesh file and to meshes in it... so if you just replace the whole text from data.ini with one from another plane.... there is a problem that can occur, than another plane has another parts, or they carry other name.....like not every plane has VertTail

 

Good luck.

 

Please, community, what are You think about? I am not sure, if i am right. :sorry::blink::biggrin:

 

EmlD

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Yep, EmlD, I think you are correct about the nodes and meshes...just swapping data inis probably wouldn't work because of this. I remember when we were doing the very early work on the N28 I used data from the SE 5 to get a working FM but I don't recall exactly how I did it. I'm thinking now I just copied some of the aerodynamic data and not the entire data.ini. :dntknw:

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Thanks EmID, that is about what I have tried. I seem to get it right in coop against AI and then it is all wrong when I fly in Dogfight. Also, Third Wire (D7 and Spad) planes seem to respond differently than the non-Third Wire (Pfalz & N28). With each patch and pack the problem/challenge seems to get worse/more difficult.

 

With the Expansion Pack the planes seem to lack energy, inspite of indicated airspeed. Is there a drag coefficient that I have been ignoring?

 

I appreciate all of the comments, thanks.

 

Personal note: Hope to see you back in the air, EmID. I have two mmp installs - one with EP and one without so should be able to join/host any game.

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Lots of work...

here is a brief (hasty) overview of what i think is the split between model/damage rigging and Flight model

Red is model/damage specific

Black could be pasted around from one craft ("normailised") YMMV

Many 3rd party planes dont have all the structure of TKs ones so there would be some fiddling

long post follows....

 

Good luck....

 

 

[MissionData]

NationName=FRANCE

ServiceStartDate=01/1917

ServiceEndDate=08/1918

AircraftRole=FIGHTER

AircraftCapability=DAY

Availability=VERY_COMMON

Exported=TRUE

ExportStartDate=04/1917

ExportEndDate=08/1918

ExportAvailability=VERY_COMMON

PrimaryRoles=SWEEP,CAP,INTERCEPT,BALLOON_BUSTING,BALLOON_DEFENSE

SecondaryRoles=CAS,RECON,ARMED_RECON,ESCORT

NormalMissionRadius=70

MaxMissionRadius=130

Ceiling=6550.0

MinBaseSize=SMALL

HasRadio=FALSE

 

[FlightControl]

StallSpeed=22.63

CruiseSpeed=45.57

ClimbSpeed=41.55

CornerSpeed=53.21

MaxG=5.20

MaxSpeedSL=57.67

MachLimit=0.169

PitchDamper=0.2

RollDamper=0.0

YawDamper=0.0

 

[DetectSystem]

MaxVisibleDistance=3600.0

 

[sound]

EngineSoundName=PropLoop

GearsSoundName=

EngineSoundPosition=0.0,1.00,0.0

 

[AircraftData]

EmptyMass=509.8

EmptyInertia=610.1,479.4,1000.9

ReferenceArea=17.84

ReferenceSpan=7.82

ReferenceChord=1.43

CGPosition=0.00,0.00,0.00

OnGroundPitchAngle=15.00

DefaultArmorType=WOOD

DefaultArmorThickness=25

Component[001]=Fuselage

Component[002]=TopWingLeft

Component[003]=TopWingRight

Component[004]=TopWingMidLeft

Component[005]=TopWingMidRight

Component[006]=TopWingTipLeft

Component[007]=TopWingTipRight

Component[008]=BottomWingLeft

Component[009]=BottomWingRight

Component[010]=BottomWingMidLeft

Component[011]=BottomWingMidRight

Component[012]=BottomWingTipLeft

Component[013]=BottomWingTipRight

Component[014]=Tail

Component[015]=LeftStab

Component[016]=RightStab

Component[017]=VertTail

Component[018]=Nose

 

[Fuselage]

ModelNodeName=Fuselage P

ShowFromCockpit=TRUE

HasAeroCoefficients=TRUE

CLa=0.0417

CD0=0.0097

CDL=0.0001

Cm0=-0.0004

Cmq=-1.4417

Cmad=-0.1377

Cyb=-0.0417

Cnb=-0.0032

CD0MachTableNumData=4

CD0MachTableDeltaX=0.10

CD0MachTableStartX=0.00

CD0MachTableData=1.672,1.126,1.000,0.937

CDLAlphaTableNumData=15

CDLAlphaTableDeltaX=4.00

CDLAlphaTableStartX=-28.00

CDLAlphaTableData=48.609,30.611,17.715,9.070,3.826,1.134,0.142,0.000,0.142,1.134,3.826,9.070,17.715,30.611,48.609

CnbAlphaTableNumData=37

CnbAlphaTableDeltaX=10.00

CnbAlphaTableStartX=-180.00

CnbAlphaTableData=-5.950,-5.897,-5.740,-5.484,-5.137,-4.709,-4.212,-3.664,-3.078,-2.475,-1.286,-1.147,-1.000,-0.856,-0.500,0.000,0.500,0.866,1.000,0.625,0.500,1.083,2.375,-1.067,-4.667,-1.533,-1.379,-2.475,-3.078,-3.664,-4.212,-4.709,-5.137,-5.484,-5.740,-5.897,-5.950

MinExtentPosition=-0.42,-2.43,-0.49

MaxExtentPosition= 0.42, 0.20, 0.61

CollisionPoint[001]=-0.33,-1.56,-0.44

CollisionPoint[002]= 0.33,-1.56,-0.44

CollisionPoint[003]= 0.00,-4.46,-0.09

CollisionPoint[004]= 0.00,-4.46, 0.34

CollisionPoint[005]= 0.00,-1.24, 0.61

CollisionPoint[006]= 0.00, 0.87, 0.36

CollisionPoint[007]=-0.41, 0.87, 0.00

CollisionPoint[008]= 0.41, 0.87, 0.00

DamageRating=DESTROYED

SystemName[001]=InternalGun

SystemName[002]=LeftMainGear

SystemName[003]=RightMainGear

SystemName[004]=MainFuelTank

SystemName[005]=Pilot

 

[Nose]

ParentComponentName=Fuselage

ModelNodeName=Nose

DestroyedNodeName=

ShowFromCockpit=TRUE

DetachWhenDestroyed=FALSE

DamageRating=DISABLED

MassFraction=0.251

HasAeroCoefficients=FALSE

MinExtentPosition=-0.44,0.20,-0.54

MaxExtentPosition= 0.44,1.17, 0.59

CollisionPoint[001]= 0.00, 1.81, 0.00

SystemName[001]=Engine

 

[TopWingLeft]

ParentComponentName=Fuselage

SupportComponentName=TopWingRight

ModelNodeName=Wing Upper Inner L

DestroyedNodeName=

ShowFromCockpit=TRUE

DetachWhenDestroyed=TRUE

DamageRating=DESTROYED

MassFraction=0.039

HasAeroCoefficients=TRUE

LiftSurface=TRUE

CL0=0.0264

CLa=0.3752

CD0=0.0037

CDL=0.0040

Cmq=-0.0848

Cmad=0.0911

Clb=-0.0025

Clp=-0.0071

Clr=0.0004

Cnp=-0.0002

Cnr=-0.0040

CL0MachTableNumData=4

CL0MachTableDeltaX=0.10

CL0MachTableStartX=0.00

CL0MachTableData=0.990,0.992,1.000,1.014

CLaMachTableNumData=4

CLaMachTableDeltaX=0.10

CLaMachTableStartX=0.00

CLaMachTableData=0.990,0.992,1.000,1.014

CD0MachTableNumData=4

CD0MachTableDeltaX=0.10

CD0MachTableStartX=0.00

CD0MachTableData=1.706,1.128,1.000,0.932

CDLAlphaTableNumData=15

CDLAlphaTableDeltaX=4.00

CDLAlphaTableStartX=-28.00

CDLAlphaTableData=8.887,6.168,3.943,2.215,0.981,0.243,0.000,0.252,1.000,2.243,3.981,6.215,8.943,12.167,15.887

CmqMachTableNumData=4

CmqMachTableDeltaX=0.10

CmqMachTableStartX=0.00

CmqMachTableData=0.960,0.965,1.000,1.055

ClbAlphaTableNumData=37

ClbAlphaTableDeltaX=10.00

ClbAlphaTableStartX=-180.00

ClbAlphaTableData=0.339,0.349,0.378,0.423,0.478,0.537,0.593,0.638,0.667,1.339,1.970,1.883,1.750,1.587,1.413,1.250,1.117,1.030,1.000,2.263,0.001,0.474,2.368,2.387,2.350,2.283,2.170,2.677,1.006,0.807,0.

93,0.537,0.478,0.423,0.378,0.349,0.339

CnrAlphaTableNumData=37

CnrAlphaTableDeltaX=10.00

CnrAlphaTableStartX=-180.00

CnrAlphaTableData=0.000,0.004,0.015,0.034,0.060,0.094,0.134,0.181,0.234,0.293,0.357,0.426,0.500,0.577,0.658,0.741,0.826,0.913,1.000,0.913,0.826,0.741,0.658,0.577,0.500,0.426,0.357,0.293,0.234,0.181,0.

34,0.094,0.060,0.034,0.015,0.004,0.000

XacMachTableNumData=4

XacMachTableDeltaX=0.10

XacMachTableStartX=0.00

XacMachTableData=-0.014,-0.014,-0.014,-0.014

CheckStall=TRUE

CLmax=0.0941

AlphaStall=7.87

AlphaMax=12.81

AlphaDepart=16.26

StallMoment=-0.001

StallDrag=0.012

StallLiftTableNumData=37

StallLiftTableDeltaX=10.00

StallLiftTableStartX=-180.00

StallLiftTableData=0.000,-0.013,-0.062,-0.239,-0.184,-0.130,-0.033,-0.047,-0.020,0.000,0.026,0.074,0.068,0.338,0.642,1.368,0.744,0.563,0.781,0.932,0.525,0.386,0.331,0.194,0.144,0.011,-0.008,-0.001,0.004,-0.006,-0.018,-0.046,-0.070,-0.050,-0.038,-0.016,0.000

StallDragTableNumData=37

StallDragTableDeltaX=10.00

StallDragTableStartX=-180.00

StallDragTableData=0.001,0.008,0.021,0.043,0.082,0.123,0.171,0.227,0.292,0.367,0.451,0.562,0.689,0.825,0.937,1.018,1.142,1.122,1.000,1.009,1.491,1.168,1.002,0.763,0.636,0.538,0.447,0.360,0.292,0.227,0

171,0.123,0.082,0.043,0.021,0.008,0.001

StallXacShiftTableNumData=37

StallXacShiftTableDeltaX=10.00

StallXacShiftTableStartX=-180.00

StallXacShiftTableData=-0.480,-0.463,-0.460,-0.350,-0.340,-0.339,-0.323,-0.301,-0.281,-0.240,-0.199,-0.179,-0.157,-0.141,-0.140,-0.126,-0.047,-0.013,0.000,-0.002,-0.002,-0.051,-0.016,0.035,0.230,0.569,0.665,0.784,-1.236,-1.232,-0.934,-0.662,-0.492,-0.439,-0.495,-0.475,-0.480

Chord=1.43

Ymac=-0.90

MinExtentPosition=-1.71,-0.97,0.77

MaxExtentPosition= 0.00, 0.46,0.87

CollisionPoint[001]=-1.71,-1.17, 0.76

CollisionPoint[002]=-1.71, 0.33, 0.82

SystemName[001]=LeftWingFuelTank

DetachNode[001]=Strut A1 L

DetachNode[002]=Strut A2 L

DetachNode[003]=Strut A3 L

DetachNode[004]=Strut B1 L

DetachNode[005]=Strut B2 L

DetachNode[006]=Strut B3 L

 

[TopWingRight]

ParentComponentName=Fuselage

SupportComponentName=TopWingLeft

ModelNodeName=Wing Upper Inner R

DestroyedNodeName=

ShowFromCockpit=TRUE

DetachWhenDestroyed=TRUE

DamageRating=DESTROYED

MassFraction=0.039

HasAeroCoefficients=TRUE

LiftSurface=TRUE

CL0=0.0264

CLa=0.3752

CD0=0.0037

CDL=0.0040

Cmq=-0.0848

Cmad=0.0911

Clb=-0.0025

Clp=-0.0071

Clr=0.0004

Cnp=-0.0002

Cnr=-0.0040

CL0MachTableNumData=4

CL0MachTableDeltaX=0.10

CL0MachTableStartX=0.00

CL0MachTableData=0.990,0.992,1.000,1.014

CLaMachTableNumData=4

CLaMachTableDeltaX=0.10

CLaMachTableStartX=0.00

CLaMachTableData=0.990,0.992,1.000,1.014

CD0MachTableNumData=4

CD0MachTableDeltaX=0.10

CD0MachTableStartX=0.00

CD0MachTableData=1.706,1.128,1.000,0.932

CDLAlphaTableNumData=15

CDLAlphaTableDeltaX=4.00

CDLAlphaTableStartX=-28.00

CDLAlphaTableData=8.887,6.168,3.943,2.215,0.981,0.243,0.000,0.252,1.000,2.243,3.981,6.215,8.943,12.167,15.887

CmqMachTableNumData=4

CmqMachTableDeltaX=0.10

CmqMachTableStartX=0.00

CmqMachTableData=0.960,0.965,1.000,1.055

ClbAlphaTableNumData=37

ClbAlphaTableDeltaX=10.00

ClbAlphaTableStartX=-180.00

ClbAlphaTableData=0.339,0.349,0.378,0.423,0.478,0.537,0.593,0.638,0.667,1.339,1.970,1.883,1.750,1.587,1.413,1.250,1.117,1.030,1.000,2.263,0.001,0.474,2.368,2.387,2.350,2.283,2.170,2.677,1.006,0.807,0.

93,0.537,0.478,0.423,0.378,0.349,0.339

CnrAlphaTableNumData=37

CnrAlphaTableDeltaX=10.00

CnrAlphaTableStartX=-180.00

CnrAlphaTableData=0.000,0.004,0.015,0.034,0.060,0.094,0.134,0.181,0.234,0.293,0.357,0.426,0.500,0.577,0.658,0.741,0.826,0.913,1.000,0.913,0.826,0.741,0.658,0.577,0.500,0.426,0.357,0.293,0.234,0.181,0.

34,0.094,0.060,0.034,0.015,0.004,0.000

XacMachTableNumData=4

XacMachTableDeltaX=0.10

XacMachTableStartX=0.00

XacMachTableData=-0.014,-0.014,-0.014,-0.014

CheckStall=TRUE

CLmax=0.0941

AlphaStall=7.87

AlphaMax=12.81

AlphaDepart=16.26

StallMoment=-0.001

StallDrag=0.012

StallLiftTableNumData=37

StallLiftTableDeltaX=10.00

StallLiftTableStartX=-180.00

StallLiftTableData=0.000,-0.013,-0.062,-0.239,-0.184,-0.130,-0.033,-0.047,-0.020,0.000,0.026,0.074,0.068,0.338,0.642,1.368,0.744,0.563,0.781,0.932,0.525,0.386,0.331,0.194,0.144,0.011,-0.008,-0.001,0.004,-0.006,-0.018,-0.046,-0.070,-0.050,-0.038,-0.016,0.000

StallDragTableNumData=37

StallDragTableDeltaX=10.00

StallDragTableStartX=-180.00

StallDragTableData=0.001,0.008,0.021,0.043,0.082,0.123,0.171,0.227,0.292,0.367,0.451,0.562,0.689,0.825,0.937,1.018,1.142,1.122,1.000,1.009,1.491,1.168,1.002,0.763,0.636,0.538,0.447,0.360,0.292,0.227,0

171,0.123,0.082,0.043,0.021,0.008,0.001

StallXacShiftTableNumData=37

StallXacShiftTableDeltaX=10.00

StallXacShiftTableStartX=-180.00

StallXacShiftTableData=-0.480,-0.463,-0.460,-0.350,-0.340,-0.339,-0.323,-0.301,-0.281,-0.240,-0.199,-0.179,-0.157,-0.141,-0.140,-0.126,-0.047,-0.013,0.000,-0.002,-0.002,-0.051,-0.016,0.035,0.230,0.569,0.665,0.784,-1.236,-1.232,-0.934,-0.662,-0.492,-0.439,-0.495,-0.475,-0.480

Chord=1.43

Ymac=0.90

MinExtentPosition= 1.71,-0.97,0.77

MaxExtentPosition= 0.00, 0.46,0.87

CollisionPoint[001]= 1.71,-1.17, 0.76

CollisionPoint[002]= 1.71, 0.33, 0.82

SystemName[001]=RightWingFuelTank

DetachNode[001]=Strut A1 R

DetachNode[002]=Strut A2 R

DetachNode[003]=Strut A3 R

DetachNode[004]=Strut B1 R

DetachNode[005]=Strut B2 R

DetachNode[006]=Strut B3 R

 

[TopWingMidLeft]

ParentComponentName=TopWingLeft

SupportComponentName=BottomWingMidLeft

ModelNodeName=Wing Upper Middle L

DestroyedNodeName=D Wing Upper Middle L

ShowFromCockpit=TRUE

DetachWhenDestroyed=TRUE

DamageRating=DISABLED

MassFraction=0.026

HasAeroCoefficients=TRUE

LiftSurface=TRUE

CL0=0.0276

CLa=0.3915

CD0=0.0025

CDL=0.0035

Cmq=-0.0573

Cmad=0.2470

Clb=-0.0017

Clp=-0.0425

Clr=0.0030

Cnp=-0.0008

Cnr=-0.0229

CL0MachTableNumData=4

CL0MachTableDeltaX=0.10

CL0MachTableStartX=0.00

CL0MachTableData=0.983,0.987,1.000,1.023

CLaMachTableNumData=4

CLaMachTableDeltaX=0.10

CLaMachTableStartX=0.00

CLaMachTableData=0.983,0.987,1.000,1.023

CD0MachTableNumData=4

CD0MachTableDeltaX=0.10

CD0MachTableStartX=0.00

CD0MachTableData=1.706,1.128,1.000,0.932

CDLAlphaTableNumData=15

CDLAlphaTableDeltaX=4.00

CDLAlphaTableStartX=-28.00

CDLAlphaTableData=8.887,6.168,3.943,2.215,0.981,0.243,0.000,0.252,1.000,2.243,3.981,6.215,8.943,12.167,15.887

CmqMachTableNumData=4

CmqMachTableDeltaX=0.10

CmqMachTableStartX=0.00

CmqMachTableData=0.960,0.965,1.000,1.055

ClbAlphaTableNumData=37

ClbAlphaTableDeltaX=10.00

ClbAlphaTableStartX=-180.00

ClbAlphaTableData=0.340,0.350,0.379,0.424,0.480,0.539,0.594,0.639,0.669,1.340,1.970,1.883,1.750,1.587,1.413,1.250,1.117,1.030,1.000,2.263,0.001,0.474,2.368,2.387,2.350,2.283,2.170,2.679,1.009,0.809,0.

94,0.539,0.480,0.424,0.379,0.350,0.340

CnrAlphaTableNumData=37

CnrAlphaTableDeltaX=10.00

CnrAlphaTableStartX=-180.00

CnrAlphaTableData=0.000,0.004,0.015,0.034,0.060,0.094,0.134,0.181,0.234,0.293,0.357,0.426,0.500,0.577,0.658,0.741,0.826,0.913,1.000,0.913,0.826,0.741,0.658,0.577,0.500,0.426,0.357,0.293,0.234,0.181,0.

34,0.094,0.060,0.034,0.015,0.004,0.000

XacMachTableNumData=4

XacMachTableDeltaX=0.10

XacMachTableStartX=0.00

XacMachTableData=-0.014,-0.014,-0.014,-0.014

CheckStall=TRUE

CLmax=0.0982

AlphaStall=7.87

AlphaMax=12.81

AlphaDepart=16.26

StallMoment=-0.001

StallDrag=0.008

StallLiftTableNumData=37

StallLiftTableDeltaX=10.00

StallLiftTableStartX=-180.00

StallLiftTableData=0.000,-0.013,-0.062,-0.239,-0.184,-0.130,-0.033,-0.047,-0.020,0.000,0.026,0.074,0.068,0.338,0.642,1.368,0.744,0.563,0.781,0.932,0.525,0.386,0.331,0.194,0.144,0.011,-0.008,-0.001,0.004,-0.006,-0.018,-0.046,-0.070,-0.050,-0.038,-0.016,0.000

StallDragTableNumData=37

StallDragTableDeltaX=10.00

StallDragTableStartX=-180.00

StallDragTableData=0.001,0.008,0.021,0.043,0.082,0.123,0.171,0.227,0.292,0.367,0.451,0.562,0.689,0.825,0.937,1.018,1.142,1.122,1.000,1.009,1.491,1.168,1.002,0.763,0.636,0.538,0.447,0.360,0.292,0.227,0

171,0.123,0.082,0.043,0.021,0.008,0.001

StallXacShiftTableNumData=37

StallXacShiftTableDeltaX=10.00

StallXacShiftTableStartX=-180.00

StallXacShiftTableData=-0.480,-0.463,-0.460,-0.350,-0.340,-0.339,-0.323,-0.301,-0.281,-0.240,-0.199,-0.179,-0.157,-0.141,-0.140,-0.126,-0.047,-0.013,0.000,-0.002,-0.002,-0.051,-0.016,0.035,0.230,0.569,0.665,0.784,-1.236,-1.232,-0.934,-0.662,-0.492,-0.439,-0.495,-0.475,-0.480

Chord=1.43

Ymac=-2.41

MinExtentPosition=-3.01,-0.97,0.77

MaxExtentPosition=-1.71, 0.46,0.87

CollisionPoint[001]=-3.01,-1.17, 0.76

CollisionPoint[002]=-3.01, 0.33, 0.82

DetachNode[001]=Strut C1 L

DetachNode[002]=Strut C2 L

RemoveNode[001]=Wires Outer L

RemoveNode[002]=Wires Inner L

////Right side removed-------------------------------------------------------

 

[bottomWingLeft]

ParentComponentName=Fuselage

ModelNodeName=Wing Lower Inner L

DestroyedNodeName=D Wing Lower Inner L

ShowFromCockpit=TRUE

DetachWhenDestroyed=TRUE

DamageRating=DESTROYED

MassFraction=0.026

HasAeroCoefficients=TRUE

LiftSurface=TRUE

CL0=0.0221

CLa=0.3337

CD0=0.0025

CDL=0.0032

Cmq=-0.0709

Cmad=0.0544

Cyb=-0.0067

Clb=-0.0113

Clp=-0.0070

Clr=0.0004

Cnp=-0.0002

Cnr=-0.0033

CL0MachTableNumData=4

CL0MachTableDeltaX=0.10

CL0MachTableStartX=0.00

CL0MachTableData=0.990,0.992,1.000,1.014

CLaMachTableNumData=4

CLaMachTableDeltaX=0.10

CLaMachTableStartX=0.00

CLaMachTableData=0.990,0.992,1.000,1.014

CD0MachTableNumData=4

CD0MachTableDeltaX=0.10

CD0MachTableStartX=0.00

CD0MachTableData=1.704,1.128,1.000,0.933

CDLAlphaTableNumData=15

CDLAlphaTableDeltaX=4.00

CDLAlphaTableStartX=-28.00

CDLAlphaTableData=9.665,6.735,4.333,2.459,1.112,0.292,0.001,0.237,1.000,2.291,4.110,6.456,9.330,12.731,16.660

CmqMachTableNumData=4

CmqMachTableDeltaX=0.10

CmqMachTableStartX=0.00

CmqMachTableData=0.960,0.965,1.000,1.055

ClbAlphaTableNumData=37

ClbAlphaTableDeltaX=10.00

ClbAlphaTableStartX=-180.00

ClbAlphaTableData=0.803,0.827,0.897,1.004,1.134,1.274,1.405,1.512,1.582,1.803,1.970,1.883,1.750,1.587,1.413,1.250,1.117,1.030,1.000,2.263,0.001,0.474,2.368,2.387,2.350,2.283,2.170,3.606,2.384,1.913,1.

05,1.274,1.134,1.004,0.897,0.827,0.803

CnrAlphaTableNumData=37

CnrAlphaTableDeltaX=10.00

CnrAlphaTableStartX=-180.00

CnrAlphaTableData=0.000,0.004,0.015,0.034,0.060,0.094,0.134,0.181,0.234,0.293,0.357,0.426,0.500,0.577,0.658,0.741,0.826,0.913,1.000,0.913,0.826,0.741,0.658,0.577,0.500,0.426,0.357,0.293,0.234,0.181,0.

34,0.094,0.060,0.034,0.015,0.004,0.000

XacMachTableNumData=4

XacMachTableDeltaX=0.10

XacMachTableStartX=0.00

XacMachTableData=0.001,0.001,0.002,0.003

CheckStall=TRUE

CLmax=0.0826

AlphaStall=7.97

AlphaMax=12.83

AlphaDepart=16.28

StallMoment=-0.001

StallDrag=0.010

StallLiftTableNumData=37

StallLiftTableDeltaX=10.00

StallLiftTableStartX=-180.00

StallLiftTableData=0.000,0.013,-0.026,0.106,0.155,0.127,0.058,-0.003,-0.001,0.000,0.002,0.013,-0.039,-0.235,-0.469,-0.566,0.350,-0.532,0.764,0.807,0.641,0.415,0.337,0.240,0.160,0.106,0.054,0.005,-0.021,-0.047,-0.069,-0.084,-0.084,-0.059,-0.041,-0.015,0.000

StallDragTableNumData=37

StallDragTableDeltaX=10.00

StallDragTableStartX=-180.00

StallDragTableData=0.001,0.008,0.021,0.043,0.082,0.123,0.171,0.227,0.292,0.367,0.451,0.562,0.689,0.825,0.937,1.018,1.142,1.122,1.000,1.009,1.491,1.168,1.002,0.763,0.636,0.538,0.447,0.360,0.292,0.227,0

171,0.123,0.082,0.043,0.021,0.008,0.001

StallXacShiftTableNumData=37

StallXacShiftTableDeltaX=10.00

StallXacShiftTableStartX=-180.00

StallXacShiftTableData=-0.519,-0.517,-0.512,-0.459,-0.495,-0.547,-0.747,-1.094,-1.177,0.747,0.740,0.738,0.427,0.158,0.001,-0.050,0.008,-0.005,0.000,-0.017,-0.023,-0.139,-0.149,-0.152,-0.169,-0.194,-0.217,-0.259,-0.302,-0.325,-0.349,-0.367,-0.370,-0.384,-0.465,-0.506,-0.519

Chord=1.27

Ymac=-0.90

MinExtentPosition=-1.71,-0.86,-0.41

MaxExtentPosition=-0.41, 0.41,-0.31

CollisionPoint[001]=-1.71, 0.29,-0.37

CollisionPoint[002]=-1.71,-1.13,-0.41

DetachNode[001]=Strut B1 L

DetachNode[002]=Strut B2 L

DetachNode[003]=Strut B3 L

 

[bottomWingRight]

ParentComponentName=Fuselage

ModelNodeName=Wing Lower Inner R

DestroyedNodeName=D Wing Lower Inner R

ShowFromCockpit=TRUE

DetachWhenDestroyed=TRUE

DamageRating=DESTROYED

MassFraction=0.026

HasAeroCoefficients=TRUE

LiftSurface=TRUE

CL0=0.0221

CLa=0.3337

CD0=0.0025

CDL=0.0032

Cmq=-0.0709

Cmad=0.0544

Cyb=-0.0067

Clb=-0.0113

Clp=-0.0070

Clr=0.0004

Cnp=-0.0002

Cnr=-0.0033

CL0MachTableNumData=4

CL0MachTableDeltaX=0.10

CL0MachTableStartX=0.00

CL0MachTableData=0.990,0.992,1.000,1.014

CLaMachTableNumData=4

CLaMachTableDeltaX=0.10

CLaMachTableStartX=0.00

CLaMachTableData=0.990,0.992,1.000,1.014

CD0MachTableNumData=4

CD0MachTableDeltaX=0.10

CD0MachTableStartX=0.00

CD0MachTableData=1.704,1.128,1.000,0.933

CDLAlphaTableNumData=15

CDLAlphaTableDeltaX=4.00

CDLAlphaTableStartX=-28.00

CDLAlphaTableData=9.665,6.735,4.333,2.459,1.112,0.292,0.001,0.237,1.000,2.291,4.110,6.456,9.330,12.731,16.660

CmqMachTableNumData=4

CmqMachTableDeltaX=0.10

CmqMachTableStartX=0.00

CmqMachTableData=0.960,0.965,1.000,1.055

ClbAlphaTableNumData=37

ClbAlphaTableDeltaX=10.00

ClbAlphaTableStartX=-180.00

ClbAlphaTableData=0.803,0.827,0.897,1.004,1.134,1.274,1.405,1.512,1.582,1.803,1.970,1.883,1.750,1.587,1.413,1.250,1.117,1.030,1.000,2.263,0.001,0.474,2.368,2.387,2.350,2.283,2.170,3.606,2.384,1.913,1.

05,1.274,1.134,1.004,0.897,0.827,0.803

CnrAlphaTableNumData=37

CnrAlphaTableDeltaX=10.00

CnrAlphaTableStartX=-180.00

CnrAlphaTableData=0.000,0.004,0.015,0.034,0.060,0.094,0.134,0.181,0.234,0.293,0.357,0.426,0.500,0.577,0.658,0.741,0.826,0.913,1.000,0.913,0.826,0.741,0.658,0.577,0.500,0.426,0.357,0.293,0.234,0.181,0.

34,0.094,0.060,0.034,0.015,0.004,0.000

XacMachTableNumData=4

XacMachTableDeltaX=0.10

XacMachTableStartX=0.00

XacMachTableData=0.001,0.001,0.002,0.003

CheckStall=TRUE

CLmax=0.0826

AlphaStall=7.97

AlphaMax=12.83

AlphaDepart=16.28

StallMoment=-0.001

StallDrag=0.010

StallLiftTableNumData=37

StallLiftTableDeltaX=10.00

StallLiftTableStartX=-180.00

StallLiftTableData=0.000,0.013,-0.026,0.106,0.155,0.127,0.058,-0.003,-0.001,0.000,0.002,0.013,-0.039,-0.235,-0.469,-0.566,0.350,-0.532,0.764,0.807,0.641,0.415,0.337,0.240,0.160,0.106,0.054,0.005,-0.021,-0.047,-0.069,-0.084,-0.084,-0.059,-0.041,-0.015,0.000

StallDragTableNumData=37

StallDragTableDeltaX=10.00

StallDragTableStartX=-180.00

StallDragTableData=0.001,0.008,0.021,0.043,0.082,0.123,0.171,0.227,0.292,0.367,0.451,0.562,0.689,0.825,0.937,1.018,1.142,1.122,1.000,1.009,1.491,1.168,1.002,0.763,0.636,0.538,0.447,0.360,0.292,0.227,0

171,0.123,0.082,0.043,0.021,0.008,0.001

StallXacShiftTableNumData=37

StallXacShiftTableDeltaX=10.00

StallXacShiftTableStartX=-180.00

StallXacShiftTableData=-0.519,-0.517,-0.512,-0.459,-0.495,-0.547,-0.747,-1.094,-1.177,0.747,0.740,0.738,0.427,0.158,0.001,-0.050,0.008,-0.005,0.000,-0.017,-0.023,-0.139,-0.149,-0.152,-0.169,-0.194,-0.217,-0.259,-0.302,-0.325,-0.349,-0.367,-0.370,-0.384,-0.465,-0.506,-0.519

Chord=1.27

Ymac=0.90

MinExtentPosition= 1.71,-0.86,-0.41

MaxExtentPosition= 0.41, 0.41,-0.31

CollisionPoint[001]= 1.71, 0.29,-0.37

CollisionPoint[002]= 1.71,-1.13,-0.41

DetachNode[001]=Strut B1 R

DetachNode[002]=Strut B2 R

DetachNode[003]=Strut B3 R

 

[bottomWingMidLeft]

ParentComponentName=BottomWingLeft

ModelNodeName=Wing Lower Middle L

DestroyedNodeName=D Wing Lower Middle L

ShowFromCockpit=TRUE

DetachWhenDestroyed=TRUE

DamageRating=DISABLED

MassFraction=0.023

HasAeroCoefficients=TRUE

LiftSurface=TRUE

CL0=0.0227

CLa=0.3427

CD0=0.0022

CDL=0.0028

Cmq=-0.0434

Cmad=0.2068

Clb=-0.0045

Clp=-0.0405

Clr=0.0027

Cnp=-0.0007

Cnr=-0.0187

CL0MachTableNumData=4

CL0MachTableDeltaX=0.10

CL0MachTableStartX=0.00

CL0MachTableData=0.982,0.986,1.000,1.025

CLaMachTableNumData=4

CLaMachTableDeltaX=0.10

CLaMachTableStartX=0.00

CLaMachTableData=0.982,0.986,1.000,1.025

CD0MachTableNumData=4

CD0MachTableDeltaX=0.10

CD0MachTableStartX=0.00

CD0MachTableData=1.704,1.128,1.000,0.933

CDLAlphaTableNumData=15

CDLAlphaTableDeltaX=4.00

CDLAlphaTableStartX=-28.00

CDLAlphaTableData=9.665,6.735,4.333,2.459,1.112,0.292,0.001,0.237,1.000,2.291,4.110,6.456,9.330,12.731,16.660

CmqMachTableNumData=4

CmqMachTableDeltaX=0.10

CmqMachTableStartX=0.00

CmqMachTableData=0.960,0.965,1.000,1.055

ClbAlphaTableNumData=37

ClbAlphaTableDeltaX=10.00

ClbAlphaTableStartX=-180.00

ClbAlphaTableData=0.695,0.715,0.776,0.868,0.982,1.102,1.216,1.308,1.368,1.695,1.970,1.883,1.750,1.587,1.413,1.250,1.117,1.030,1.000,2.263,0.001,0.474,2.368,2.387,2.350,2.283,2.170,3.389,2.063,1.655,1.

16,1.102,0.982,0.868,0.776,0.715,0.695

CnrAlphaTableNumData=37

CnrAlphaTableDeltaX=10.00

CnrAlphaTableStartX=-180.00

CnrAlphaTableData=0.000,0.004,0.015,0.034,0.060,0.094,0.134,0.181,0.234,0.293,0.357,0.426,0.500,0.577,0.658,0.741,0.826,0.913,1.000,0.913,0.826,0.741,0.658,0.577,0.500,0.426,0.357,0.293,0.234,0.181,0.

34,0.094,0.060,0.034,0.015,0.004,0.000

XacMachTableNumData=4

XacMachTableDeltaX=0.10

XacMachTableStartX=0.00

XacMachTableData=-0.042,-0.042,-0.043,-0.044

CheckStall=TRUE

CLmax=0.0849

AlphaStall=7.97

AlphaMax=12.83

AlphaDepart=16.28

StallMoment=-0.001

StallDrag=0.007

StallLiftTableNumData=37

StallLiftTableDeltaX=10.00

StallLiftTableStartX=-180.00

StallLiftTableData=0.000,0.013,-0.026,0.106,0.155,0.127,0.058,-0.003,-0.001,0.000,0.002,0.013,-0.039,-0.235,-0.469,-0.566,0.350,-0.532,0.764,0.807,0.641,0.415,0.337,0.240,0.160,0.106,0.054,0.005,-0.021,-0.047,-0.069,-0.084,-0.084,-0.059,-0.041,-0.015,0.000

StallDragTableNumData=37

StallDragTableDeltaX=10.00

StallDragTableStartX=-180.00

StallDragTableData=0.001,0.008,0.021,0.043,0.082,0.123,0.171,0.227,0.292,0.367,0.451,0.562,0.689,0.825,0.937,1.018,1.142,1.122,1.000,1.009,1.491,1.168,1.002,0.763,0.636,0.538,0.447,0.360,0.292,0.227,0

171,0.123,0.082,0.043,0.021,0.008,0.001

StallXacShiftTableNumData=37

StallXacShiftTableDeltaX=10.00

StallXacShiftTableStartX=-180.00

StallXacShiftTableData=-0.448,-0.447,-0.452,-0.405,-0.442,-0.495,-0.699,-1.050,-1.138,0.782,0.771,0.765,0.450,0.177,0.018,-0.034,0.019,-0.005,0.000,-0.017,-0.013,-0.123,-0.132,-0.133,-0.147,-0.168,-0.185,-0.224,-0.263,-0.281,-0.302,-0.316,-0.316,-0.330,-0.405,-0.436,-0.448

Chord=1.27

Ymac=-2.41

MinExtentPosition=-3.01,-0.86,-0.41

MaxExtentPosition=-1.71, 0.41,-0.31

CollisionPoint[001]=-3.01, 0.29,-0.37

CollisionPoint[002]=-3.01,-1.13,-0.41

DetachNode[001]=Bell Crank Pivot L

DetachNode[002]=Bell Crank Frame L

////Right side removed-------------------------------------------------------

 

[Tail]

ParentComponentName=Fuselage

ModelNodeName=Tail

DestroyedNodeName=D Tail

ShowFromCockpit=TRUE

DetachWhenDestroyed=TRUE

DamageRating=DESTROYED

HasAeroCoefficients=FALSE

MinExtentPosition=-0.15,-4.16,-0.19

MaxExtentPosition= 0.15,-2.43, 0.46

CollisionPoint[001]= 0.00,-4.45,-0.10

SystemName[001]=TailGear

 

[VertTail]

ParentComponentName=Tail

ModelNodeName=Vertical Stabilizer

DestroyedNodeName=D Vertical Stabilizer

ShowFromCockpit=TRUE

DetachWhenDestroyed=TRUE

DamageRating=DESTROYED

MassFraction=0.038

HasAeroCoefficients=TRUE

CD0=0.0008

Cyb=-0.0339

Cyp=0.0024

Cyr=0.0346

Clb=-0.0006

Clp=-0.0001

Clr=0.0006

Cnb=0.0173

Cnp=-0.0012

Cnr=-0.0177

CD0MachTableNumData=4

CD0MachTableDeltaX=0.10

CD0MachTableStartX=0.00

CD0MachTableData=1.709,1.133,1.000,0.941

CnbAlphaTableNumData=37

CnbAlphaTableDeltaX=10.00

CnbAlphaTableStartX=-180.00

CnbAlphaTableData=1.113,1.133,1.191,1.280,1.389,1.505,1.614,1.703,1.761,1.691,1.582,1.530,1.450,1.352,1.248,1.150,1.070,1.018,1.000,0.940,1.067,-0.098,-0.478,-0.034,0.066,0.140,0.185,0.211,0.249,0.327,0.445,0.591,0.745,0.891,1.009,1.087,1.113

CnrAlphaTableNumData=37

CnrAlphaTableDeltaX=10.00

CnrAlphaTableStartX=-180.00

CnrAlphaTableData=0.631,0.641,0.631,0.595,0.530,0.435,0.318,0.192,0.080,0.006,-0.004,-0.003,0.028,0.113,0.267,0.477,0.704,0.892,1.000,0.972,0.844,0.642,0.422,0.233,0.104,0.036,0.011,0.006,0.008,0.068,0.167,0.281,0.389,0.481,0.552,0.601,0.631

MinExtentPosition=-0.03,-4.76,0.44

MaxExtentPosition= 0.03,-3.35,1.08

CollisionPoint[001]= 0.00,-5.00, 1.03

CollisionPoint[002]= 0.00,-4.59, 1.03

SystemName[001]=Rudder

RemoveNode[001]=Tail Wire L

RemoveNode[002]=Tail Wire R

 

[LeftStab]

ParentComponentName=Tail

ModelNodeName=Horizontal Stabilizer L

DestroyedNodeName=D Horizontal Stabilizer L

ShowFromCockpit=TRUE

DetachWhenDestroyed=TRUE

DamageRating=DISABLED

MassFraction=0.020

HasAeroCoefficients=TRUE

LiftSurface=TRUE

CL0=0.0092

CLa=0.1891

CD0=0.0017

CDL=0.0005

Cmq=-2.8692

Cmad=-0.9245

Cyb=-0.0258

Clp=-0.0012

Cnb=0.0123

CL0MachTableNumData=4

CL0MachTableDeltaX=0.10

CL0MachTableStartX=0.00

CL0MachTableData=-4.435,-0.926,1.000,0.229

CLaMachTableNumData=4

CLaMachTableDeltaX=0.10

CLaMachTableStartX=0.00

CLaMachTableData=0.989,0.992,1.000,1.014

CD0MachTableNumData=4

CD0MachTableDeltaX=0.10

CD0MachTableStartX=0.00

CD0MachTableData=1.699,1.133,1.000,0.937

CDLAlphaTableNumData=15

CDLAlphaTableDeltaX=4.00

CDLAlphaTableStartX=-28.00

CDLAlphaTableData=49.000,36.000,25.000,16.000,9.000,4.000,1.000,0.000,1.000,4.000,9.000,16.000,25.000,36.000,49.000

CmqMachTableNumData=4

CmqMachTableDeltaX=0.10

CmqMachTableStartX=0.00

CmqMachTableData=0.990,0.992,1.000,1.014

XacMachTableNumData=4

XacMachTableDeltaX=0.10

XacMachTableStartX=0.00

XacMachTableData=-3.731,-3.731,-3.731,-3.730

CheckStall=TRUE

CLmax=0.0527

AlphaStall=15.31

AlphaMax=21.59

AlphaDepart=28.40

StallMoment=0.000

StallDrag=0.000

StallLiftTableNumData=37

StallLiftTableDeltaX=10.00

StallLiftTableStartX=-180.00

StallLiftTableData=0.000,-0.018,-0.036,-0.059,-0.080,-0.075,-0.065,-0.044,-0.019,0.000,0.024,0.069,0.131,0.195,0.281,0.341,0.474,0.739,1.000,0.815,0.504,0.368,0.293,0.232,0.165,0.103,0.053,0.000,-0.019,-0.044,-0.065,-0.075,-0.080,-0.059,-0.036,-0.018,0.000

StallDragTableNumData=37

StallDragTableDeltaX=10.00

StallDragTableStartX=-180.00

StallDragTableData=0.001,0.008,0.021,0.043,0.082,0.123,0.171,0.227,0.292,0.367,0.451,0.562,0.689,0.825,0.937,1.018,1.142,1.122,1.000,1.122,1.142,1.018,0.937,0.825,0.689,0.562,0.451,0.367,0.292,0.227,0

171,0.123,0.082,0.043,0.021,0.008,0.001

StallXacShiftTableNumData=37

StallXacShiftTableDeltaX=10.00

StallXacShiftTableStartX=-180.00

StallXacShiftTableData=-0.519,-0.519,-0.444,-0.400,-0.395,-0.380,-0.353,-0.325,-0.287,-0.260,-0.232,-0.194,-0.166,-0.140,-0.124,-0.120,-0.075,0.000,0.000,0.000,-0.075,-0.120,-0.124,-0.140,-0.166,-0.194,-0.232,-0.260,-0.287,-0.325,-0.353,-0.380,-0.395,-0.400,-0.444,-0.519,-0.519

DownwashAlphaTableNumData=37

DownwashAlphaTableDeltaX=10.00

DownwashAlphaTableStartX=-180.00

DownwashAlphaTableData=0.000,0.000,0.000,0.000,0.000,0.000,0.000,0.000,0.000,-0.021,-0.177,-0.697,-1.766,-3.517,-5.532,-6.355,-4.870,-1.920,1.281,4.062,6.766,8.747,7.951,4.942,2.257,0.765,0.143,0.026,0.000,0.000,0.000,0.000,0.000,0.000,0.000,0.000,0.000

Chord=0.92

Ymac=-0.59

MinExtentPosition=-1.32,-4.30,0.38

MaxExtentPosition=-0.05,-3.37,0.43

CollisionPoint[001]=-1.44,-4.10, 0.32

CollisionPoint[002]=-1.52,-4.29, 0.32

SystemName[001]=LeftElevator

DetachNode[001]=Horizontal Stabilizer Brace L

RemoveNode[001]=Tail Wire L

////Right side removed-------------------------------------------------------

 

// Crew ---------------------------------------------------------

 

[Pilot]

SystemType=PILOT_COCKPIT

PilotModelName=wwiPilotNewF

PilotHeadNodeName=head

Position=0.00,-0.707,0.639

MinExtentPosition=-0.29,-0.87,-0.16

MaxExtentPosition= 0.29,-0.37, 0.70

 

// Engines ---------------------------------------------------------

 

[Engine]

SystemType=PROP_ENGINE

InputName=THROTTLE_CONTROL

EngineID=1

SLPowerDry=134226.0

ThrustAngles=0.0,0.0,0.0

ThrustPosition=0.0,0.0,0.0

ThrottleRate=0.5

AltitudeTableNumData=10

AltitudeTableDeltaX=914.4

AltitudeTableStartX=0.0

AltitudeTableData=1.000,0.925,0.854,0.787,0.724,0.664,0.609,0.557,0.508,0.000

NumBlades=2

PropDiameter=2.46

MomentOfInertia=4.06

PropEfficiencyAdvanceRatioTableNumData=12

PropEfficiencyAdvanceRatioTableDeltaX=0.1

PropEfficiencyAdvanceRatioTableStartX=0.0

PropEfficiencyAdvanceRatioTableData=0.044,0.309,0.512,0.620,0.734,0.772,0.799,0.800,0.800,0.695,0.447,0.000

ConstantSpeed=FALSE

SpinnerNodeName=Prop Axle

StaticPropNodeName=Prop Static

SlowPropNodeName=Prop Slow Hub

FastPropNodeName=Prop Fast Hub

DamagedPropNodeName=D Prop Static

SlowPropRPM=400

FastPropRPM=800

MaxPropRPM=1800

IdlePropRPM=500

BSFC=0.00280

ExhaustEmitterName=InlineExhaustEmitter

ExhaustPosition=0.0,-1.76,0.04

FireSuppression=FALSE

MinExtentPosition=-0.40,0.48,-0.40

MaxExtentPosition= 0.40,1.13, 0.40

MinManifoldPressure=0.33

MaxManifoldPressure=1.00

GasTempIdleRPM=60

GasTempMaxRPM=80

GasTempChangeRate=0.1

OverheatTemp=100

DamageTempDelta=20

OverheatDamageRate=

OilPressIdleRPM=5.10

OilPressMaxRPM=4.08

OilPressChangeRate=0.07

LowOilPress=2.04

LowOilPressTempDelta=100

AnimationID=6

MaxPowerAnimationTime=0.1

MinPowerAnimationTime=0.2

 

// Control Surfaces ---------------------------------------------------------

 

[LeftElevator]

SystemType=CONTROL_SURFACE

InputName=PITCH_CONTROL

MaxDeflection=20.0

MinDeflection=-30.0

CLiftdc=0.0723

CDdc=0.0058

Cmdc=-0.1890

CLiftdcAlphaTableNumData=37

CLiftdcAlphaTableDeltaX=10.00

CLiftdcAlphaTableStartX=-180.00

CLiftdcAlphaTableData=0.000,-0.014,-0.029,-0.047,-0.064,-0.060,-0.052,-0.035,-0.015,0.000,0.019,0.055,0.104,0.155,0.224,0.636,1.000,1.000,1.000,1.000,1.000,0.646,0.233,0.185,0.131,0.082,0.042,0.000,-0.015,-0.035,-0.052,-0.060,-0.064,-0.047,-0.029,-0.014,0.000

CmdcAlphaTableNumData=37

CmdcAlphaTableDeltaX=10.00

CmdcAlphaTableStartX=-180.00

CmdcAlphaTableData=0.000,-0.014,-0.029,-0.047,-0.064,-0.060,-0.052,-0.035,-0.015,0.000,0.019,0.055,0.104,0.155,0.224,0.636,1.000,1.000,1.000,1.000,1.000,0.646,0.233,0.185,0.131,0.082,0.042,0.000,-0.015,-0.035,-0.052,-0.060,-0.064,-0.047,-0.029,-0.014,0.000

MaxControlSpeed=54.09

ControlRate=5.0

ModelNodeName=Elevator L

ReverseModelOrientation=TRUE

////Right side removed-------------------------------------------------------

 

[LeftAileron]

SystemType=CONTROL_SURFACE

InputName=ROLL_CONTROL

MaxDeflection=30.0

MinDeflection=-30.0

CDdc=0.0209

Cldc=0.0649

Cndc=-0.0023

CldcAlphaTableNumData=37

CldcAlphaTableDeltaX=10.00

CldcAlphaTableStartX=-180.00

CldcAlphaTableData=1.000,0.940,0.766,0.500,0.174,-0.174,-0.500,-0.766,-0.940,-1.000,-0.940,-0.766,-0.500,-0.174,0.174,0.500,0.766,0.940,1.000,0.912,0.882,0.838,0.368,0.147,0.059,-0.766,-0.940,-1.000,-0.940,-0.766,-0.500,-0.174,0.174,0.500,0.766,0.940,1.000

CndcAlphaTableNumData=37

CndcAlphaTableDeltaX=10.00

CndcAlphaTableStartX=-180.00

CndcAlphaTableData=1.000,0.940,0.766,0.500,0.174,-0.174,-0.500,-0.766,-0.940,-1.000,-0.940,-0.766,-0.500,-0.174,0.174,0.500,0.766,0.940,1.000,0.811,0.000,-0.585,-0.453,-1.226,-1.736,-1.666,-1.540,-1.300,-1.090,-0.816,-0.500,-0.174,0.174,0.500,0.766,0.940,1.000

MaxControlSpeed=53.21

ControlRate=5.0

ModelNodeName=Aileron L

AnimationID=1

DetachNode[001]=Bell Crank Push Rod L

////Right side removed-------------------------------------------------------

 

 

[Rudder]

SystemType=CONTROL_SURFACE

InputName=YAW_CONTROL

ReverseInput=TRUE

MaxDeflection=30.0

MinDeflection=-30.0

CDdc=0.0124

Cydc=0.0560

Cldc=0.0010

Cndc=-0.0286

CydcAlphaTableNumData=37

CydcAlphaTableDeltaX=10.00

CydcAlphaTableStartX=-180.00

CydcAlphaTableData=1.000,0.970,0.883,0.750,0.587,0.413,0.250,0.117,0.030,0.000,0.030,0.117,0.250,0.413,0.587,0.750,0.883,0.970,1.000,0.970,0.883,0.750,0.587,0.413,0.250,0.117,0.030,0.000,0.030,0.117,0

250,0.413,0.587,0.750,0.883,0.970,1.000

CldcAlphaTableNumData=37

CldcAlphaTableDeltaX=10.00

CldcAlphaTableStartX=-180.00

CldcAlphaTableData=-1.000,-0.985,-0.940,-0.866,-0.766,-0.643,-0.500,-0.342,-0.174,0.000,0.174,0.342,0.500,0.643,0.766,0.866,0.940,0.985,1.000,1.040,0.871,0.643,0.339,0.170,0.201,0.140,0.185,0.200,0.224,0.294,0.400,0.531,0.669,0.800,0.906,0.976,1.000

CndcAlphaTableNumData=37

CndcAlphaTableDeltaX=10.00

CndcAlphaTableStartX=-180.00

CndcAlphaTableData=-1.000,-0.985,-0.940,-0.866,-0.766,-0.643,-0.500,-0.342,-0.174,0.000,0.174,0.342,0.500,0.643,0.766,0.866,0.940,0.985,1.000,0.971,0.986,0.990,0.718,0.163,0.000,0.000,0.000,0.000,0.112,0.294,0.400,0.531,0.669,0.800,0.906,0.976,1.000

MaxControlSpeed=53.21

ControlRate=5.0

ModelNodeName=Rudder

AnimationID=2

RemoveNode[001]=Rudder Wire L

RemoveNode[002]=Rudder Wire R

 

// Internal Guns ---------------------------------------------------------

 

[internalGun]

SystemType=FIXED_GUN

GunTypeName=303CAL_VICKERS_MK1

InputName=FIRE_PRIMARY_GUN

GunGroup=1

MuzzlePosition=0.06,0.80,0.51

LightPosition= 0.06,0.85,0.51

AimAngles=0.8,0.0,0.0

MaxAmmo=380

EjectShells=TRUE

EjectPosition=-0.45,-0.25,-0.24

EjectVelocity=-0.5,-1.0,-0.0

MinExtentPosition=0.01,-0.25,0.46

MaxExtentPosition=0.12, 0.80,0.59

GunFireAnimationID=7

Synchronized=TRUE

 

// Weapon Stations ---------------------------------------------------------

 

// Fuel Tanks ---------------------------------------------------------

 

[MainFuelTank]

SystemType=FUEL_TANK

FuelTankID=1

MaxFuelAmount=34.03

SelfHealing=FALSE

FireSuppression=FALSE

MinExtentPosition=-0.36,-0.77,-0.54

MaxExtentPosition= 0.36, 0.20,-0.37

 

[LeftWingFuelTank]

SystemType=FUEL_TANK

FuelTankID=2

MaxFuelAmount=20.00

SelfHealing=FALSE

FireSuppression=FALSE

MinExtentPosition=-0.28,-0.27,0.81

MaxExtentPosition= 0.00, 0.42,0.87

////Right side removed-------------------------------------------------------

 

// Landing Gears ---------------------------------------------------------

 

[LeftMainGear]

SystemType=LANDING_GEAR

Retractable=FALSE

ModelNodeName=Gear Strut L

ShockAnimationID=4

ShockStroke=0.07

SpringFactor=1.3

DampingFactor=2.0

WheelNodeName=Wheel L

RotationAxis=Z-Axis

RollingRadius=0.35

CastoringWheel=FALSE

RollingCoefficient=0.30

MaxLoadFactor=4.0

////Right side removed-------------------------------------------------------

 

[TailGear]

SystemType=LANDING_GEAR

Retractable=FALSE

IsSkid=TRUE

HideGearNode=FALSE

ModelNodeName=Skid

ShockAnimationID=3

ShockStroke=0.05

SpringFactor=1.3

DampingFactor=1.8

ContactPoint=0.00,-3.84,-0.37

RollingCoefficient=0.70

MaxLoadFactor=6.0

 

 

// Airbrakes ---------------------------------------------------------

 

// Lights ---------------------------------------------------------

 

//-----------------------------------------------------------------------------

 

Edited by p10ppy

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Thanks p10ppy. A lot to digest. I will start work right after this post. This will save me alot of time. Again, thanks. Any other suggestions would be appreciated.

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