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## Ignore Visual Studio temporary files, build results, and | ||
## files generated by popular Visual Studio add-ons. | ||
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# User-specific files | ||
*.suo | ||
*.user | ||
*.sln.docstates | ||
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# Build results | ||
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[Dd]ebug/ | ||
[Rr]elease/ | ||
x64/ | ||
build/ | ||
[Bb]in/ | ||
[Oo]bj/ | ||
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||
# Enable "build/" folder in the NuGet Packages folder since NuGet packages use it for MSBuild targets | ||
!packages/*/build/ | ||
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||
# MSTest test Results | ||
[Tt]est[Rr]esult*/ | ||
[Bb]uild[Ll]og.* | ||
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*_i.c | ||
*_p.c | ||
*.ilk | ||
*.meta | ||
*.pch | ||
*.pdb | ||
*.pgc | ||
*.pgd | ||
*.rsp | ||
*.sbr | ||
*.tlb | ||
*.tli | ||
*.tlh | ||
*.tmp | ||
*.tmp_proj | ||
*.log | ||
*.vspscc | ||
*.vssscc | ||
.builds | ||
*.pidb | ||
*.log | ||
*.scc | ||
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||
# Visual C++ cache files | ||
ipch/ | ||
*.aps | ||
*.ncb | ||
*.opensdf | ||
*.sdf | ||
*.cachefile | ||
|
||
# Visual Studio profiler | ||
*.psess | ||
*.vsp | ||
*.vspx | ||
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||
# Guidance Automation Toolkit | ||
*.gpState | ||
|
||
# ReSharper is a .NET coding add-in | ||
_ReSharper*/ | ||
*.[Rr]e[Ss]harper | ||
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||
# TeamCity is a build add-in | ||
_TeamCity* | ||
|
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# DotCover is a Code Coverage Tool | ||
*.dotCover | ||
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# NCrunch | ||
*.ncrunch* | ||
.*crunch*.local.xml | ||
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# Installshield output folder | ||
[Ee]xpress/ | ||
|
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# DocProject is a documentation generator add-in | ||
DocProject/buildhelp/ | ||
DocProject/Help/*.HxT | ||
DocProject/Help/*.HxC | ||
DocProject/Help/*.hhc | ||
DocProject/Help/*.hhk | ||
DocProject/Help/*.hhp | ||
DocProject/Help/Html2 | ||
DocProject/Help/html | ||
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# Click-Once directory | ||
publish/ | ||
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# Publish Web Output | ||
*.Publish.xml | ||
*.pubxml | ||
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# NuGet Packages Directory | ||
## TODO: If you have NuGet Package Restore enabled, uncomment the next line | ||
#packages/ | ||
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# Windows Azure Build Output | ||
csx | ||
*.build.csdef | ||
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# Windows Store app package directory | ||
AppPackages/ | ||
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# Others | ||
sql/ | ||
*.Cache | ||
ClientBin/ | ||
[Ss]tyle[Cc]op.* | ||
~$* | ||
*~ | ||
*.dbmdl | ||
*.[Pp]ublish.xml | ||
*.pfx | ||
*.publishsettings | ||
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# RIA/Silverlight projects | ||
Generated_Code/ | ||
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# Backup & report files from converting an old project file to a newer | ||
# Visual Studio version. Backup files are not needed, because we have git ;-) | ||
_UpgradeReport_Files/ | ||
Backup*/ | ||
UpgradeLog*.XML | ||
UpgradeLog*.htm | ||
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# SQL Server files | ||
App_Data/*.mdf | ||
App_Data/*.ldf | ||
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# ========================= | ||
# Windows detritus | ||
# ========================= | ||
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# Windows image file caches | ||
Thumbs.db | ||
ehthumbs.db | ||
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# Folder config file | ||
Desktop.ini | ||
|
||
# Recycle Bin used on file shares | ||
$RECYCLE.BIN/ | ||
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# Mac crap | ||
.DS_Store |
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PWingsSettings | ||
{ | ||
keyTranslation = g | ||
keyTipScale = t | ||
keyRootScale = b | ||
moveSpeed = 5 | ||
scaleSpeed = 0.25 | ||
} |
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PART | ||
{ | ||
// --- general parameters --- | ||
name = Proceduralwing2 | ||
module = Winglet | ||
author = DYJ | ||
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// --- asset parameters --- | ||
mesh = model.mu | ||
scale = 1 | ||
rescaleFactor = 1 | ||
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// --- editor parameters --- | ||
TechRequired = advAerodynamics | ||
entryCost = 10000 | ||
cost = 0 | ||
category = Aero | ||
subcategory = 0 | ||
title = PWing - Mark 2 | ||
manufacturer = Procedural Dynamics | ||
description = Wing part of yet to be determined shape, size, mass and other measurements aswell. | ||
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// attachment rules: stack, srfAttach, allowStack, allowSrfAttach, allowCollision | ||
attachRules = 0,1,0,1,1 | ||
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// --- node definitions --- | ||
// definition format is Position X, Position Y, Position Z, Up X, Up Y, Up Z | ||
node_attach = 0.0, 0.0, 0.0, -1.0, 0.0, 0.0 | ||
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// --- standard part parameters --- | ||
mass = 0.033 | ||
dragModelType = override | ||
maximum_drag = 0.02 | ||
minimum_drag = 0.02 | ||
angularDrag = 2 | ||
crashTolerance = 15 | ||
maxTemp = 1700 | ||
explosionPotential = 0.1 | ||
fuelCrossFeed = True | ||
breakingTorque = 100 | ||
breakingForce = 100 | ||
mirrorRefAxis = 0, 0, -1 | ||
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// --- winglet parameters --- | ||
// dragCoeff will override the maximum_drag value | ||
dragCoeff = 0.2 | ||
deflectionLiftCoeff = 0.5 | ||
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MODULE | ||
{ | ||
name = WingManipulator | ||
} | ||
} | ||
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@PART[Proceduralwing2]:NEEDS[FerramAerospaceResearch|NEAR] { | ||
@module = Part | ||
@maximum_drag = 0 | ||
@minimum_drag = 0 | ||
@angularDrag = 0 | ||
!dragCoeff = DELETE | ||
!deflectionLiftCoeff = DELETE | ||
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MODULE | ||
{ | ||
name = FARWingAerodynamicModel | ||
MAC = 2 | ||
MidChordSweep = 0 | ||
b_2 = 1 | ||
TaperRatio = 1 | ||
} | ||
} |
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71 changes: 71 additions & 0 deletions
71
ProceduralDynamics/Parts/DYJproceduralwing2endcap/part.cfg
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PART | ||
{ | ||
// --- general parameters --- | ||
name = Proceduralwing2EndPiece | ||
module = Winglet | ||
author = DYJ | ||
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// --- asset parameters --- | ||
mesh = model.mu | ||
scale = 1 | ||
rescaleFactor = 1 | ||
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// --- editor parameters --- | ||
TechRequired = advAerodynamics | ||
entryCost = 10000 | ||
cost = 0 | ||
category = Aero | ||
subcategory = 0 | ||
title = PWing - Mark2 Tip | ||
manufacturer = Procedural Dynamics | ||
description = Wing part of yet to be determined shape, size, mass and other measurements aswell, this one is rounder than the others. | ||
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// attachment rules: stack, srfAttach, allowStack, allowSrfAttach, allowCollision | ||
attachRules = 0,1,0,1,1 | ||
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// --- node definitions --- | ||
// definition format is Position X, Position Y, Position Z, Up X, Up Y, Up Z | ||
node_attach = 0.0, 0.0, 0.0, -1.0, 0.0, 0.0 | ||
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// --- standard part parameters --- | ||
mass = 0.033 | ||
dragModelType = override | ||
maximum_drag = 0.02 | ||
minimum_drag = 0.02 | ||
angularDrag = 2 | ||
crashTolerance = 15 | ||
maxTemp = 1700 | ||
explosionPotential = 0.1 | ||
fuelCrossFeed = True | ||
breakingTorque = 100 | ||
breakingForce = 100 | ||
mirrorRefAxis = 0, 0, -1 | ||
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// --- winglet parameters --- | ||
// dragCoeff will override the maximum_drag value | ||
dragCoeff = 0.2 | ||
deflectionLiftCoeff = 0.5 | ||
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MODULE | ||
{ | ||
name = WingManipulator | ||
} | ||
} | ||
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@PART[Proceduralwing2EndPiece]:NEEDS[FerramAerospaceResearch|NEAR] { | ||
@module = Part | ||
@maximum_drag = 0 | ||
@minimum_drag = 0 | ||
@angularDrag = 0 | ||
!dragCoeff = DELETE | ||
!deflectionLiftCoeff = DELETE | ||
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MODULE | ||
{ | ||
name = FARWingAerodynamicModel | ||
MAC = 2 | ||
MidChordSweep = 0 | ||
b_2 = 1 | ||
TaperRatio = 1 | ||
} | ||
} |
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PART | ||
{ | ||
// --- general parameters --- | ||
name = Proceduralwing4 | ||
module = Winglet | ||
author = DYJ | ||
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// --- asset parameters --- | ||
mesh = model.mu | ||
scale = 1 | ||
rescaleFactor = 1 | ||
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// --- editor parameters --- | ||
TechRequired = advAerodynamics | ||
entryCost = 10000 | ||
cost = 0 | ||
category = Aero | ||
subcategory = 0 | ||
title = PWing - Mark 4 | ||
manufacturer = Procedural Dynamics | ||
description = Wing part of yet to be determined shape, size, mass and other measurements aswell. | ||
|
||
// attachment rules: stack, srfAttach, allowStack, allowSrfAttach, allowCollision | ||
attachRules = 0,1,0,1,1 | ||
|
||
// --- node definitions --- | ||
// definition format is Position X, Position Y, Position Z, Up X, Up Y, Up Z | ||
node_attach = 0.0, 0.0, 0.0, -1.0, 0.0, 0.0 | ||
|
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// --- standard part parameters --- | ||
mass = 0.033 | ||
dragModelType = override | ||
maximum_drag = 0.02 | ||
minimum_drag = 0.02 | ||
angularDrag = 2 | ||
crashTolerance = 15 | ||
maxTemp = 1700 | ||
explosionPotential = 0.1 | ||
fuelCrossFeed = True | ||
breakingTorque = 100 | ||
breakingForce = 100 | ||
mirrorRefAxis = 0, 0, -1 | ||
|
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// --- winglet parameters --- | ||
// dragCoeff will override the maximum_drag value | ||
dragCoeff = 0.2 | ||
deflectionLiftCoeff = 0.5 | ||
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MODULE | ||
{ | ||
name = WingManipulator | ||
} | ||
|
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MODULE | ||
{ | ||
name = FlapToggler | ||
} | ||
} | ||
|
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@PART[Proceduralwing4]:NEEDS[FerramAerospaceResearch|NEAR] { | ||
@module = Part | ||
@maximum_drag = 0 | ||
@minimum_drag = 0 | ||
@angularDrag = 0 | ||
!dragCoeff = DELETE | ||
!deflectionLiftCoeff = DELETE | ||
|
||
MODULE | ||
{ | ||
name = FARWingAerodynamicModel | ||
MAC = 2 | ||
MidChordSweep = 0 | ||
b_2 = 1 | ||
TaperRatio = 1 | ||
} | ||
} |
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ProceduralDynamics/Parts/DYJproceduralwingAllMovingSurface/model000.png
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