Draft: importAirfoilDAT, improved spacing around operators
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@@ -30,12 +30,19 @@ __author__ = "Heiko Jakob <heiko.jakob@gediegos.de>"
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#
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# This module provides support for importing airfoil .dat files
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import re, FreeCAD, FreeCADGui, Part, cProfile, os, string
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import re, FreeCAD, Part, cProfile, os
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from FreeCAD import Vector, Base
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from FreeCAD import Console as FCC
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from Draft import makeWire
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if open.__module__ in ['__builtin__','io']:
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pythonopen = open
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if FreeCAD.GuiUp:
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from DraftTools import translate
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else:
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def translate(context, txt):
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return txt
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if open.__module__ in ['__builtin__', 'io']:
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pythonopen = open
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useDraftWire = True
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@@ -65,7 +72,9 @@ def decodeName(name):
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try:
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decodedName = (name.decode("utf8"))
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except UnicodeDecodeError:
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print("AirfoilDAT: error: couldn't determine character encoding")
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_msg = ("AirfoilDAT error: "
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"couldn't determine character encoding.")
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FCC.PrintError(translate("ImportAirfoilDAT", _msg) + "\n")
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decodedName = name
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return decodedName
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@@ -86,7 +95,7 @@ def open(filename):
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docname = os.path.splitext(os.path.basename(filename))[0]
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doc = FreeCAD.newDocument(docname)
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doc.Label = decodeName(docname[:-4])
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process(doc,filename)
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process(doc, filename)
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def insert(filename,docname):
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@@ -110,15 +119,15 @@ def insert(filename,docname):
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"""
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groupname = os.path.splitext(os.path.basename(filename))[0]
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try:
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doc=FreeCAD.getDocument(docname)
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doc = FreeCAD.getDocument(docname)
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except NameError:
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doc=FreeCAD.newDocument(docname)
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importgroup = doc.addObject("App::DocumentObjectGroup",groupname)
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doc = FreeCAD.newDocument(docname)
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importgroup = doc.addObject("App::DocumentObjectGroup", groupname)
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importgroup.Label = decodeName(groupname)
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process(doc,filename)
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process(doc, filename)
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def process(doc,filename):
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def process(doc, filename):
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"""Process the filename and provide the document with the information.
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The common airfoil dat format has many flavors.
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@@ -140,26 +149,26 @@ def process(doc,filename):
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"""
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# Regex to identify data rows and throw away unused metadata
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regex = re.compile(r'^\s*(?P<xval>(\-|\d*)\.\d+(E\-?\d+)?)\,?\s*(?P<yval>\-?\s*\d*\.\d+(E\-?\d+)?)\s*$')
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afile = pythonopen(filename,'r')
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afile = pythonopen(filename, 'r')
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# read the airfoil name which is always at the first line
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airfoilname = afile.readline().strip()
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coords=[]
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upside=True
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last_x=None
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coords = []
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upside = True
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last_x = None
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# Collect the data for the upper and the lower side separately if possible
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for lin in afile:
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curdat = regex.match(lin)
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if curdat != None:
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if curdat is not None:
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x = float(curdat.group("xval"))
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y = float(curdat.group("yval"))
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# the normal processing
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coords.append(Vector(x,y,0))
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coords.append(Vector(x, y, 0))
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# End of if curdat != None
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# End of for lin in file
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@@ -173,7 +182,7 @@ def process(doc,filename):
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# sometimes coords are divided in upper an lower side
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# so that x-coordinate begin new from leading or trailing edge
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# check for start coordinates in the middle of list
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# check for start coordinates in the middle of list
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if coords[0:-1].count(coords[0]) > 1:
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flippoint = coords.index(coords[0],1)
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@@ -187,7 +196,7 @@ def process(doc,filename):
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# do we use the parametric Draft Wire?
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if useDraftWire:
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obj = makeWire ( coords, True )
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obj = makeWire(coords, True)
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#obj.label = airfoilname
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else:
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# alternate solution, uses common Part Faces
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@@ -200,7 +209,7 @@ def process(doc,filename):
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# End of if first_v == None
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# Line between v and last_v if they're not equal
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if (last_v != None) and (last_v != v):
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if (last_v is not None) and (last_v != v):
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lines.append(Part.makeLine(last_v, v))
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# End of if (last_v != None) and (last_v != v)
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# The new last_v
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