def neuralGrow(poistion, angle, length, maxangledeviation, generation,
maxgeneration):
goal = rs.Polar(poistion, angle, length)
rs.AddCone(goal, poistion, 11 - generation)
angle1 = angle + random.uniform(-maxangledeviation, -5)
angle2 = angle + random.uniform(5, maxangledeviation)
if generation < maxgeneration:
neuralGrow(goal, angle1, length, maxangledeviation, generation + 1,
maxgeneration)
neuralGrow(goal, angle2, length, maxangledeviation, generation + 1,
maxgeneration)
# modified from RhinoPythonPrimer Rev3
import rhinoscriptsyntax as rs
import time
rs.AddCone((0, 0, 0), 10, 5, True)
strObjectID = rs.GetObject("select an obj to rename", 0, False, True)
if strObjectID:
strNewName = "Time: " + str(time.localtime())
rs.ObjectName(strObjectID, strNewName)
# alt = rs.ObjectName(strObjectID, "time: " & str(time.localtime()))
print strNewName
# Clear the board
rs.DeleteObjects(rs.AllObjects(select=True))
rabbit = Prey()
rabbit.penup()
rabbit.position = Point3d(20, 40, 0)
rabbit.color = Color.Blue
rabbit.pendown()
fox = Predator(8)
fox.color = Color.Red
rabbitIcon = rs.AddSphere(rabbit.position, 0.5)
rs.ObjectColor(rabbitIcon, rabbit.color)
rabbit.decorate(rhinoturtle.Decorator(rabbitIcon))
foxIcon = rs.AddCone(Plane.WorldXY, 2, 1)
rs.ObjectColor(foxIcon, fox.color)
fox.decorate(rhinoturtle.Decorator(foxIcon))
caught = False
while not caught:
rabbit.wander()
caught = fox.chase(rabbit)
rs.Sleep(500)
rs.DeleteObject(rabbitIcon)
phi = k * dphi
x = (R + a * (ma.cos(n * phi) - 1)) * ma.cos(phi)
y = (R + a * (ma.cos(n * phi) - 1)) * ma.sin(phi)
points.append([x, y, z])
sections.append(rs.AddInterpCurve(points))
top = rs.EvaluateCurve(curve, domain[1])
plane = rs.PlaneFromNormal(top, [0, 0, 1])
sections.append(rs.AddCircle(plane, 1))
rs.AddLayer("Cactus")
rs.CurrentLayer("Cactus")
surf = rs.AddLoftSrf(sections)
rs.CapPlanarHoles(surf)
#Draw spines
cone = rs.AddCone([0, 0, -sh], sh, sr)
basis = []
theta = ma.pi / 8
dphi = 2 * ma.pi / m
for k in range(0, m):
phi = k * dphi
x = ma.sin(theta) * ma.cos(phi)
y = ma.sin(theta) * ma.sin(phi)
z = ma.cos(theta)
matrix = rs.XformRotation3([0, 0, 1], [x, y, z], [0, 0, 0])
basis.append(rs.TransformObject(cone, matrix, True))
rs.DeleteObject(cone)
for crv in ridges:
domain = rs.CurveDomain(crv)
dt = (domain[1] - domain[0]) / 10
import rhinoscriptsyntax as rs Radius = 50 radius = 3.0 height = 100 rs.AddCone((0, 0, 0), height, Radius, True) rs.AddCylinder((20, 0, 0), height, Radius, True) rs.AddSphere((40, 0, 6), Radius) rs.AddTorus((60, 0, 3), Radius, radius)
def TurbofanNacelle(EngineSection,
Chord,
CentreLocation=[0, 0, 0],
ScarfAngle=3,
HighlightRadius=1.45,
MeanNacelleLength=5.67):
# The defaults yield a nacelle similar to that of an RR Trent 1000 / GEnx
HighlightDepth = 0.12 * MeanNacelleLength
SectionNo = 100
# Draw the nacelle with the centre of the intake highlight circle in 0,0,0
rs.EnableRedraw(False)
Highlight = rs.AddCircle3Pt((0, 0, HighlightRadius),
(0, -HighlightRadius, 0),
(0, 0, -HighlightRadius))
HighlightCutterCircle = rs.AddCircle3Pt((0, 0, HighlightRadius * 1.5),
(0, -HighlightRadius * 1.5, 0),
(0, 0, -HighlightRadius * 1.5))
# Fan disk for CFD boundary conditions
FanCircle = rs.CopyObject(Highlight, (MeanNacelleLength * 0.25, 0, 0))
FanDisk = rs.AddPlanarSrf(FanCircle)
# Aft outflow for CFD boundary conditions
BypassCircle = rs.CopyObject(Highlight, (MeanNacelleLength * 0.85, 0, 0))
BypassDisk = rs.AddPlanarSrf(BypassCircle)
rs.DeleteObjects([FanCircle, BypassCircle])
# Outflow cone
TailConeBasePoint = [MeanNacelleLength * 0.84, 0, 0]
TailConeApex = [MeanNacelleLength * 1.35, 0, 0]
TailConeRadius = HighlightRadius * 0.782
TailCone = rs.AddCone(TailConeBasePoint, TailConeApex, TailConeRadius)
# Spinner cone
SpinnerConeBasePoint = [MeanNacelleLength * 0.26, 0, 0]
SpinnerConeApex = [MeanNacelleLength * 0.08, 0, 0]
SpinnerConeRadius = MeanNacelleLength * 0.09
Spinner = rs.AddCone(SpinnerConeBasePoint, SpinnerConeApex,
SpinnerConeRadius)
# Tilt the intake
RotVec = rs.VectorCreate((0, 0, 0), (0, 1, 0))
Highlight = rs.RotateObject(Highlight, (0, 0, 0), ScarfAngle, axis=RotVec)
# Set up the disk for separating the intake lip later
HighlightCutterCircle = rs.RotateObject(HighlightCutterCircle, (0, 0, 0),
ScarfAngle,
axis=RotVec)
HighlightCutterDisk = rs.AddPlanarSrf(HighlightCutterCircle)
rs.DeleteObject(HighlightCutterCircle)
rs.MoveObject(HighlightCutterDisk, (HighlightDepth, 0, 0))
# Build the actual airfoil sections to define the nacelle
HighlightPointVector = rs.DivideCurve(Highlight, SectionNo)
Sections = []
TailPoints = []
Rotation = 0
Twist = 0
AirfoilSeligName = 'goe613'
SmoothingPasses = 1
for HighlightPoint in HighlightPointVector:
ChordLength = MeanNacelleLength - HighlightPoint.X
Af = primitives.Airfoil(HighlightPoint, ChordLength, Rotation, Twist,
airconics_setup.SeligPath)
AfCurve, Chrd = primitives.Airfoil.AddAirfoilFromSeligFile(
Af, AirfoilSeligName, SmoothingPasses)
rs.DeleteObject(Chrd)
P = rs.CurveEndPoint(AfCurve)
list.append(TailPoints, P)
AfCurve = act.AddTEtoOpenAirfoil(AfCurve)
list.append(Sections, AfCurve)
Rotation = Rotation + 360.0 / SectionNo
list.append(TailPoints, TailPoints[0])
# Build the actual nacelle OML surface
EndCircle = rs.AddInterpCurve(TailPoints)
Nacelle = rs.AddSweep2([Highlight, EndCircle], Sections, closed=True)
# Separate the lip
Cowling, HighlightSection = rs.SplitBrep(Nacelle, HighlightCutterDisk,
True)
# Now build the pylon between the engine and the specified chord on the wing
CP1 = [
MeanNacelleLength * 0.26 + CentreLocation[0], CentreLocation[1],
CentreLocation[2] + HighlightRadius * 0.1
]
CP2 = [
MeanNacelleLength * 0.4 + CentreLocation[0], CentreLocation[1],
HighlightRadius * 1.45 + CentreLocation[2]
]
CP3 = rs.CurveEndPoint(Chord)
rs.ReverseCurve(Chord)
CP4 = rs.CurveEndPoint(Chord)
# Move the engine into its actual place on the wing
rs.MoveObjects(
[HighlightSection, Cowling, FanDisk, BypassDisk, TailCone, Spinner],
CentreLocation)
# Pylon wireframe
PylonTop = rs.AddInterpCurve([CP1, CP2, CP3, CP4])
PylonAf = primitives.Airfoil(CP1, MeanNacelleLength * 1.35, 90, 0,
airconics_setup.SeligPath)
PylonAfCurve, PylonChord = primitives.Airfoil.AddNACA4(
PylonAf, 0, 0, 12, 3)
LowerTE = rs.CurveEndPoint(PylonChord)
PylonTE = rs.AddLine(LowerTE, CP4)
# Create the actual pylon surface
PylonLeft = rs.AddNetworkSrf([PylonTop, PylonAfCurve, PylonTE])
rs.MoveObject(PylonLeft, (0, -CentreLocation[1], 0))
PylonRight = act.MirrorObjectXZ(PylonLeft)
rs.MoveObject(PylonLeft, (0, CentreLocation[1], 0))
rs.MoveObject(PylonRight, (0, CentreLocation[1], 0))
PylonAfCurve = act.AddTEtoOpenAirfoil(PylonAfCurve)
PylonAfSrf = rs.AddPlanarSrf(PylonAfCurve)
# Assigning basic surface properties
act.AssignMaterial(Cowling, "ShinyBABlueMetal")
act.AssignMaterial(HighlightSection, "UnpaintedMetal")
act.AssignMaterial(TailCone, "UnpaintedMetal")
act.AssignMaterial(FanDisk, "FanDisk")
act.AssignMaterial(Spinner, "ShinyBlack")
act.AssignMaterial(BypassDisk, "FanDisk")
act.AssignMaterial(PylonLeft, "White_composite_external")
act.AssignMaterial(PylonRight, "White_composite_external")
# Clean-up
rs.DeleteObject(HighlightCutterDisk)
rs.DeleteObjects(Sections)
rs.DeleteObject(EndCircle)
rs.DeleteObject(Highlight)
rs.DeleteObjects([PylonTop, PylonAfCurve, PylonChord, PylonTE])
rs.Redraw()
TFEngine = [
Cowling, HighlightSection, TailCone, FanDisk, Spinner, BypassDisk
]
TFPylon = [PylonLeft, PylonRight, PylonAfSrf]
return TFEngine, TFPylon
import rhinoscriptsyntax as rs
import math
import random
import Rhino.Geometry as rg
for x in range(100):
for y in range(x):
for z in range(y):
rs.AddCone((x**2, y**2, z**2), )
def createConeVisual(_space):
for i in range(10):
point1 = rs.CreatePoint(i*spacing,0,0)
rs.AddCone((i*_space,0, spacing/2*random.random()), -random.randint(1,spacing), random.randint(1,spacing/2))
import rhinoscriptsyntax as rs # rs.AddPoint( - syntax tip myPoint = rs.AddPoint((1, 2, 3)) # rs.AddSphere(center, radius) myRadius = 3 mySpere = rs.AddSphere(myPoint, myRadius) # skapa en kone myCone = rs.AddCone((1, 2, 3), 20, 10) # skapa en cylinder myCone = rs.AddCylinder((0, -10, 0), 2, 10) # skapa en linje myPoint_2 = rs.AddPoint((0, 0, 0)) myPoint_3 = rs.AddPoint((10, 0, 0)) rs.AddLine(myPoint_2, myPoint_3)
import rhinoscriptsyntax as rs all = rs.AllObjects() rs.DeleteObjects(all) plane1 = rs.PlaneFromFrame([0, 0, 0], [0, 1, 0], [1, 0, 0]) plane2 = rs.PlaneFromFrame([0, 0, 6], [0, 1, 0], [1, 0, 0]) plane3 = rs.PlaneFromFrame([0, 0, 40], [0, 1, 0], [1, 0, 0]) nose = rs.AddCone(plane2, 6, 20, cap=True) nose2 = rs.AddCone(plane3, 24, 5, cap=True) hat1 = rs.AddCylinder(plane1, 110, 20, cap=True) hat2 = rs.AddCylinder(plane1, -6, 10, cap=True) hat3 = rs.AddCylinder(plane2, -10, 12, cap=True) ##neck=rs.AddCylinder ((0,0,-35), 10, 5, cap=True)
z = rs.AddPoint(0, 1, -.4) j = 0 plane11 = rs.RotatePlane(plane1, 0, [0, 1, 0]) #for i in range(50): #plane11 = rs.RotatePlane(plane1, j, [0,1,0]) #j=j+10 #rs.AddRectangle( plane11, 25.0, 25.0 ) #rs.AddCircle( plane11, 25.0 ) #rs.AddSphere ( plane11, 25.0 ) #plane11 = rs.RotatePlane(plane1, j, [0,0,1]) #j=j+10 #rs.AddRectangle( plane11, 25.0, 25.0 ) #rs.AddSphere ( plane11, 50.0 )\ head = rs.AddSphere(plane11, 25.0) eyeL = rs.AddSphere(plane2, 5.0) eyeR = rs.AddSphere(plane3, 5.0) #rs.AddSphere ( plane11, 25.0 ) #rs.AddCircle( (0,0,25), 50.0 ) hat1 = rs.AddCone(plane5, -25, 25, cap=False) nose = rs.AddCone(plane4, 15, 5, cap=True) hat2 = rs.AddCylinder(plane6, -1, 50, cap=True) hat2 = rs.AddTorus(plane6, 50, 2) neck = rs.AddCylinder((0, 0, -30), 10, 5, cap=True) #body=rs.AddCylinder ((0,0,-70), 40, 50, cap=True) body = rs.AddCylinder((0, 0, -95), 60, 30, cap=True) #body=rs.GetRectangle (4, (0,0,-130),) collar = rs.AddTorus((0, 0, -35), 15, 5)
